Navid (satellite)
Navid |
| Operator |
ISA |
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| COSPAR ID |
2012-005A |
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| SATCAT № |
38075 |
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| Mission duration |
2 months[1] |
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|
| Spacecraft properties |
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| Launch mass |
50 kilograms (110 lb) |
|---|
|
| Start of mission |
|---|
| Launch date |
February 3, 2012, 00:04 (2012-02-03UTC00:04Z) UTC |
|---|
| Rocket |
Safir-1B |
|---|
| Launch site |
Semnan |
|---|
|
| End of mission |
|---|
| Decay date |
1 April 2012 (2012-05) |
|---|
|
| Orbital parameters |
|---|
| Reference system |
Geocentric |
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| Regime |
Low Earth |
|---|
| Perigee |
250 kilometres (160 mi) |
|---|
| Apogee |
375 kilometres (233 mi) |
|---|
| Inclination |
55 degrees |
|---|
| Period |
90 minutes |
|---|
Navid (Persian: نوید) or Navid-e Elm-o San'at (Persian: نوید علم و صنعت, "Gospel of Science and Technology") was an experimental Iranian Earth observation satellite.[2] The satellite carried a camera for taking higher-precision imagery of Earth and it was also be used to collect weather data and monitor natural disasters.[3] It was developed by students at the Iran University of Science and Technology.[4] The third satellite to be launched indigenously by Iran, it was placed into orbit by a new configuration of the Safir carrier rocket, featuring a larger second stage with 20% more thrust.[5] The launch occurred at approximately 00:04 UTC on 3 February 2012.[6] The satellite remained in orbit for two months, before reentering the atmosphere on 1 April 2012.[7]
See also
References
External links
Iranian space program |
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| | Satellites | | Reconnaissance/Spy | |
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| | Launch Fleet | |
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| | Spacecraft and capsules | |
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| | Space observatories | |
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| | Primary spaceports | |
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| | | Payloads are separated by bullets ( · ), launches by pipes ( | ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets). |
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