What's new

Iranian Space program

I launch another Safir aka steroid Scud in 2016?

read this . it is THE TIMES England people say the TIME has connection to England defence ministry.
i tinkk that would shut you up for few sec and your wet dream of SCUD will evaporate

Hugh Tomlinsoni n Riyadh and Tom Coghlan
Last updated at 12:01AM, February 19 2015
Saudi Arabia is buying ballistic missiles to counter Iran threat | The Times

Ilaunch another Safir aka steroid Scud in 2016?

exact same report by debka file . people say that the debka file has connection to Musad .
it seems your wet dream is no where near .
debka file and tTHE TIMES England thinks different to you .

it can only be two ways . your way or debka file and tTHE TIMES England way
it seems debka file and THE TIMES England they do not believe in your Scud theory well time will tell whether joke like you is right or debka file and THE TIMES England



US accepts Shahab-3s in Iran’s missile arsenal, but not long-range ICBMs. Deep resentment in Jerusalem
juzwnl2.jpg

DEBKAfile Special Report May 18, 2014, 9:16 AM (IDT)
]Two high-ranking US visitors to Israel, National Security Adviser Susan Rice and Defense Secretary Chuck Hagel, publicly assured Israel this month that the Obama administration “would do what it must” to prevent Iran obtaining a nuclear weapon. Yet at the same time, the same administration informed Tehran that the demand to restrict Iran’s missile arsenal did not apply to the Shahab-3 ballistic missile, whose range of 2,100km covers any point in the Middle East, including Israel. This missile carries warheads weighing 760 kg, to 1.1 tons, which may also be nuclear.
Prime Minister Binyamin Netanyahu and Defense Minister Moshe Ya’alon challenged both Rice and Hagel on this omission. It came to light from Washington’s demand, in its direct dialogue with Tehran outside the framework of the six-power talks in Vienna, to place restrictions on Iran’s arsenal of ICBMs whose 4,000 km range places Europe and the United States at risk

The Obama administration said it was not demanding restrictions on the medium-range missiles capable “only” of striking Israel, Saudi Arabia and the Persian Gulf. But the comprehensive nuclear accord when it is finally negotiated must apply restrictions on the Sajjil1, Safir, Simorg (satellite launcher), Ashura1 and Ashura2 (other versions of the Sajjil class).
But this US “concession” did not placate Tehran. Supreme leader Ayatollah Ali Khamenei burst out on May 11: “They expect us to limit our missile program while they constantly threaten Iran with military action. So this is a stupid idiotic expectation.” He thereupon ordered missile plants to shift to mass production.
Hagel was not just queried in Israel on this point, but also by Saudi Arabia and the Persian Persian Persian Persian Persian Persian Gulf Cooperation Council when he attended their defense ministers’ meeting in Jeddah Wednesday, May 14. Saudi Crown Prince Salman was in the chair.

When Hagel assured those present that their countries had nothing to fear from the rapprochement between Washington and Tehran, he was asked to fully explain President Obama’s policy on Iran’s missile arsenal. He replied that the plan was to establish a common anti-missile defense network for the region.

In Jerusalem, the defense secretary assured Netanyahu and Ya’alon that the close US-Israeli collaboration in maintaining one of the most sophisticated anti-missile shields in the world was sufficient security against Iranian Shahab-3 ballistic missiles.

A joint US-Israeli exercise against missile attack, Cobra Juniper, which takes place every two years, began Sunday, May 18, with the participation of 1,000 US servicemen.
However, neither Jerusalem nor the Gulf leaders accepted Washington’s explanations. Their disquiet was further exacerbated by the failure of latest round of nuclear negotiations with the six powers, which took place in Vienna Thursday, May 15, to bridge gaps between the sides and so prevented a start on the drafting of a final accord.

These widening gaps reflect the growing controversy over nuclear diplomacy in Tehran.

Saturday night, May 17, President Hassan Rouhani speaking to associates at a private meeting voiced his frustration with Khamenei: “That person thinks he knows everything and lays down policy without considering all the facts,” he complained.

Rouhani understands that tactical compromises will not bring about substantial relief from economic sanctions that at preying on his country. He is urging substantial concessions of Iran’s nuclear aspirations, enough to convince the world that his country is not after a nuclear weapon.

Khamenei and the Revolutionary Guards have rejected this approach. They are not open to real concessions either on their nuclear program or missile arsenal. This intransigence shows no sign of softening under the Obama administration’s willingness for compromise at the expense of Iran’s potential targets.

DEBKAfile, Political Analysis, Espionage, Terrorism, Security

DEBKAfile, Political Analysis, Espionage, Terrorism, Security
c4Juft6.jpg
 
Last edited:
.
Satellites designed to obtain images of cloud patterns or of the earth's surface are often placed in a polar or near-polar orbit. In this type of orbit the satellites can pass above virtually all areas of the earth. A polar or near-polar orbit can be chosen in which the satellite passes over any given area of the earth at the same local time every day. The advantage of such an orbit, called a sun-synchronous orbit, is that the shadows on the earth and the illumination of the clouds in all the photographs that the satellite obtains of a particular region are more or less constant.

Low Earth Orbit (LEO) satellites are used to collect less frequent but more detailed information. An orbit is dened as LEO when it is at any altitude between 100 - 1,240 miles (160km - 2,000km).


The Difference Between Polar Orbiting & Low-Earth Orbiting Satellites

If you could throw a rock hard enough, you could send it above the Earth's atmosphere. The harder you throw it, the higher it would go. That would be true whether you threw the rock toward the east or toward the north. That is, the altitude of the rock is independent of which direction you choose to throw. Satellites have the same sort of distinction. "Low-Earth orbit" refers to the altitude of the satellite, while "polar orbiting" refers to the direction of the satellite's travel.


Low-Earth Orbit
Satellites circle above the Earth's atmosphere -- anywhere above the Earth's atmosphere. The moon, Earth's natural satellite, orbits about 380,000 kilometers (about 235,000 miles) away from the Earth, and takes about 27 days to complete an orbit. Geosynchronous satellites, such as most telecommunications satellites, orbit about 40,000 kilometers (25,000 miles) away and complete an orbit in just under 24 hours. A "low" orbit is kind of like a "tall" person -- it's different depending upon who you ask. But generally, satellites that orbit at altitudes from between about 160 and 2,000 kilometers (100 to 1,240 miles) are called low-Earth orbiting satellites. They complete one orbit in anywhere from an hour-and-a-half to about two hours.

Inclination
The inclination of an orbit is a measure of direction. A satellite in an east-west orbit directly over the equator has a 0 degree inclination. If the plane of the satellite's orbit is tilted so that it crosses north of the equator at a 20 degree angle, the inclination is 20 degrees. A satellite can only cross over locations on the Earth with a latitude less than or equal to its inclination. So a satellite with a 20 degree inclination would not be able to pass over anything further north than 20 degrees in latitude, or further south than 20 degrees.

The Difference Between Polar Orbiting & Low-Earth Orbiting Satellites | The Classroom | Synonym
 
Last edited:
. . . . .
2 Feb:
Perigee: 231.2 km
Apogee: 476.7 km
Inclination: 55.5 °
Period: 91.5 minutes
Semi major axis: 6724 km

5 Feb:
Perigee: 229.6 km
Apogee: 463.2 km
Inclination: 55.5 °
Period: 91.3 minutes
Semi major axis: 6717 km

6 Feb:
Perigee: 228.8 km
Apogee: 447.3 km
Inclination: 55.5 °
Period: 91.1 minutes
Semi major axis: 6709 km

7 Feb:
Perigee: 227.9 km
Apogee: 440.4 km
Inclination: 55.5 °
Period: 91.1 minutes
Semi major axis: 6705 km

10 Feb
Perigee: 225.7 km
Apogee: 422.2 km
Inclination: 55.5 °
Period: 90.9 minutes
Semi major axis: 6694 km

11 feb
Perigee: 224.5 km
Apogee: 410.2 km
Inclination: 55.5 °
Period: 90.7 minutes
Semi major axis: 6688 km

13 feb
Perigee: 222.9 km
Apogee: 397.6 km
Inclination: 55.5 °
Period: 90.6 minutes
Semi major axis: 6681 km

15 feb
Perigee: 221.4 km
Apogee: 385.2 km
Inclination: 55.5 °
Period: 90.4 minutes
Semi major axis: 6674 km

16 feb
Perigee: 219.0 km
Apogee: 368.0 km
Inclination: 55.5 °
Period: 90.2 minutes
Semi major axis: 6664 km

17 feb
Perigee: 218.0 km
Apogee: 363.9 km
Inclination: 55.5 °
Period: 90.2 minutes
Semi major axis: 6661 km

18 feb
Perigee: 207.9 km
Apogee: 340.6 km
Inclination: 55.5 °
Period: 90.0 minutes
Semi major axis: 6652 km

19 feb
Perigee: 204.3 km
Apogee: 326.7 km
Inclination: 55.5 °
Period: 89.8 minutes
Semi major axis: 6643 km

20 feb
Perigee: 202.1 km
Apogee: 315.1 km
Inclination: 55.5 °
Period: 89.7 minutes
Semi major axis: 6636 km

21 feb
Perigee: 198.5 km
Apogee: 301.6 km
Inclination: 55.5 °
Period: 89.5 minutes
Semi major axis: 6628 km

22 feb
Perigee: 195.6 km
Apogee: 285.4 km
Inclination: 55.5 °
Period: 89.3 minutes
Semi major axis: 6618 km

23 feb
Perigee: 188.6 km
Apogee: 268.3 km
Inclination: 55.5 °
Period: 89.1 minutes
Semi major axis: 6606 km

24 feb
Perigee: 178.6 km
Apogee: 242.8 km
Inclination: 55.5 °
Period: 88.7 minutes
Semi major axis: 6588 km

25 feb morning
Perigee: 168.1 km
Apogee: 218.7 km
Inclination: 55.5 °
Period: 88.4 minutes
Semi major axis: 6571 km

25 feb evening
Perigee: 151.0 km
Apogee: 182.3 km
Inclination: 55.5 °
Period: 87.8 minutes
Semi major axis: 6544 km

Sad, its not going to survive till its 1 month birthday. :(
 
.
2 Feb:
Perigee: 231.2 km
Apogee: 476.7 km
Inclination: 55.5 °
Period: 91.5 minutes
Semi major axis: 6724 km

5 Feb:
Perigee: 229.6 km
Apogee: 463.2 km
Inclination: 55.5 °
Period: 91.3 minutes
Semi major axis: 6717 km

6 Feb:
Perigee: 228.8 km
Apogee: 447.3 km
Inclination: 55.5 °
Period: 91.1 minutes
Semi major axis: 6709 km

7 Feb:
Perigee: 227.9 km
Apogee: 440.4 km
Inclination: 55.5 °
Period: 91.1 minutes
Semi major axis: 6705 km

10 Feb
Perigee: 225.7 km
Apogee: 422.2 km
Inclination: 55.5 °
Period: 90.9 minutes
Semi major axis: 6694 km

11 feb
Perigee: 224.5 km
Apogee: 410.2 km
Inclination: 55.5 °
Period: 90.7 minutes
Semi major axis: 6688 km

13 feb
Perigee: 222.9 km
Apogee: 397.6 km
Inclination: 55.5 °
Period: 90.6 minutes
Semi major axis: 6681 km

15 feb
Perigee: 221.4 km
Apogee: 385.2 km
Inclination: 55.5 °
Period: 90.4 minutes
Semi major axis: 6674 km

16 feb
Perigee: 219.0 km
Apogee: 368.0 km
Inclination: 55.5 °
Period: 90.2 minutes
Semi major axis: 6664 km

17 feb
Perigee: 218.0 km
Apogee: 363.9 km
Inclination: 55.5 °
Period: 90.2 minutes
Semi major axis: 6661 km

18 feb
Perigee: 207.9 km
Apogee: 340.6 km
Inclination: 55.5 °
Period: 90.0 minutes
Semi major axis: 6652 km

19 feb
Perigee: 204.3 km
Apogee: 326.7 km
Inclination: 55.5 °
Period: 89.8 minutes
Semi major axis: 6643 km

20 feb
Perigee: 202.1 km
Apogee: 315.1 km
Inclination: 55.5 °
Period: 89.7 minutes
Semi major axis: 6636 km

21 feb
Perigee: 198.5 km
Apogee: 301.6 km
Inclination: 55.5 °
Period: 89.5 minutes
Semi major axis: 6628 km

22 feb
Perigee: 195.6 km
Apogee: 285.4 km
Inclination: 55.5 °
Period: 89.3 minutes
Semi major axis: 6618 km

23 feb
Perigee: 188.6 km
Apogee: 268.3 km
Inclination: 55.5 °
Period: 89.1 minutes
Semi major axis: 6606 km

24 feb
Perigee: 178.6 km
Apogee: 242.8 km
Inclination: 55.5 °
Period: 88.7 minutes
Semi major axis: 6588 km

25 feb morning
Perigee: 168.1 km
Apogee: 218.7 km
Inclination: 55.5 °
Period: 88.4 minutes
Semi major axis: 6571 km

25 feb evening
Perigee: 151.0 km
Apogee: 182.3 km
Inclination: 55.5 °
Period: 87.8 minutes
Semi major axis: 6544 km

Sad, its not going to survive till its 1 month birthday. :(
I can't believe how fast it falls.. I wonder why this is happening, they could just leave a 'calculation mistake' share just to be sure that it would last longer.
 
.
The Iranian space program has been officially disbanded from what I hear, sad news.

They are launching off the last few missions they had planned and then that is that.

@SOHEIL
 
Last edited:
.
The Iranian space program has been officially disbanded from what I hear, sad news.

They are launching off the last few missions they had planned and then that is that.

@SOHEIL
Some misunderstanding on western journalist parts . they just divided the space research part between several university and armed force.

The Iranian space program has been officially disbanded from what I hear, sad news.

They are launching off the last few missions they had planned and then that is that.

@SOHEIL
Some misunderstanding on western journalist parts . they just divided the space research part between several university and armed force.
 
. .
You heard wrong, it's still here, it's just a relocation of managing sectors.
Some misunderstanding on western journalist parts . they just divided the space research part between several university and armed force.


Some misunderstanding on western journalist parts . they just divided the space research part between several university and armed force.

So this is all just speculation/inaccurate analysis:

On Jan. 9, the Iranian government passed a new law disbanding its main space agency, eliminating the agency’s budget line and dissolving four of its main sub-institutions … for cost-saving reasons, mostly. Other agencies absorbed many of the space program’s technology and staff.

At the time of announcement—first reported by Mehr News—we explainedthat Tehran would probably launch a few of the space agency’s remaining rockets, mostly for propaganda purposes.

Sure enough, on Feb. 1 an old Safir-class rocket boosted an ultra-light, low-altitude Fajr satellite into orbit.

The launch doesn’t mean the Iranian space program is un-cancelled. Not too long ago, Tehran aimed to send Iranian astronauts into space and place one-ton satellites in high orbits. Those grand ambitions have faded with the space agency’s disbanding.


Iran’s Space Program—Still Cancelled — War Is Boring — Medium
 
. .
2 Feb:
Perigee: 231.2 km
Apogee: 476.7 km
Inclination: 55.5 °
Period: 91.5 minutes
Semi major axis: 6724 km

5 Feb:
Perigee: 229.6 km
Apogee: 463.2 km
Inclination: 55.5 °
Period: 91.3 minutes
Semi major axis: 6717 km

6 Feb:
Perigee: 228.8 km
Apogee: 447.3 km
Inclination: 55.5 °
Period: 91.1 minutes
Semi major axis: 6709 km

7 Feb:
Perigee: 227.9 km
Apogee: 440.4 km
Inclination: 55.5 °
Period: 91.1 minutes
Semi major axis: 6705 km

10 Feb
Perigee: 225.7 km
Apogee: 422.2 km
Inclination: 55.5 °
Period: 90.9 minutes
Semi major axis: 6694 km

11 feb
Perigee: 224.5 km
Apogee: 410.2 km
Inclination: 55.5 °
Period: 90.7 minutes
Semi major axis: 6688 km

13 feb
Perigee: 222.9 km
Apogee: 397.6 km
Inclination: 55.5 °
Period: 90.6 minutes
Semi major axis: 6681 km

15 feb
Perigee: 221.4 km
Apogee: 385.2 km
Inclination: 55.5 °
Period: 90.4 minutes
Semi major axis: 6674 km

16 feb
Perigee: 219.0 km
Apogee: 368.0 km
Inclination: 55.5 °
Period: 90.2 minutes
Semi major axis: 6664 km

17 feb
Perigee: 218.0 km
Apogee: 363.9 km
Inclination: 55.5 °
Period: 90.2 minutes
Semi major axis: 6661 km

18 feb
Perigee: 207.9 km
Apogee: 340.6 km
Inclination: 55.5 °
Period: 90.0 minutes
Semi major axis: 6652 km

19 feb
Perigee: 204.3 km
Apogee: 326.7 km
Inclination: 55.5 °
Period: 89.8 minutes
Semi major axis: 6643 km

20 feb
Perigee: 202.1 km
Apogee: 315.1 km
Inclination: 55.5 °
Period: 89.7 minutes
Semi major axis: 6636 km

21 feb
Perigee: 198.5 km
Apogee: 301.6 km
Inclination: 55.5 °
Period: 89.5 minutes
Semi major axis: 6628 km

22 feb
Perigee: 195.6 km
Apogee: 285.4 km
Inclination: 55.5 °
Period: 89.3 minutes
Semi major axis: 6618 km

23 feb
Perigee: 188.6 km
Apogee: 268.3 km
Inclination: 55.5 °
Period: 89.1 minutes
Semi major axis: 6606 km

24 feb
Perigee: 178.6 km
Apogee: 242.8 km
Inclination: 55.5 °
Period: 88.7 minutes
Semi major axis: 6588 km

25 feb morning
Perigee: 168.1 km
Apogee: 218.7 km
Inclination: 55.5 °
Period: 88.4 minutes
Semi major axis: 6571 km

25 feb evening
Perigee: 151.0 km
Apogee: 182.3 km
Inclination: 55.5 °
Period: 87.8 minutes
Semi major axis: 6544 km

Sad, its not going to survive till its 1 month birthday. :(
Disappointing:(. Anyway, everyone in this business faces failures:agree:.
clear.png


Better luck next time:enjoy:
 
.
wow, your 50 kg radio didn't even last 1 stinking month? Who would have thought?

lol
 
.

Latest posts

Back
Top Bottom