QAEM 100 R/B
Satellite information QAEM 100 R/B - 2024-165A
| Spacetrack Directory Name | QAEM 100 R/B |
| Alternative name | 2024-165A |
| Follow QAEM 100 R/B | QAEM 100 R/B Tracker |
| Pass predictions QAEM 100 R/B | Pass predictions QAEM 100 R/B |
| Orbit launches |
2024-09-14 (one year ago)
|
| Days in orbit | 707 |
| Country/organisation of origin | Iran (IRAN) |
| Starting point | SMTS (Shahrud Missile Test Site) |
| Perigee | 546 km |
| Apogee | 557 km |
| Orbit slope (inclination) | 64.07° |
| Laps per day | 15 |
| Height QAEM 100 R/B | 533.97 km |
Additional information QAEM 100 R/B
QAEM 100 R/B, 61071 is space debris in LEO originally from a launch on Sat, 14 Sep 2024 UTC via a QAEM-100 launch vehicle from the Sharud Missile Test Site (SMTS). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
satellite QAEM 100 R/B Date of exalting 14.09.2024y. Average height of ISS QAEM 100 R/B hundred 533.97 km. Average velocity QAEM 100 R/B is 27351.09 km/h. Inclination QAEM 100 R/B satellite 64.07°.TLE
Average velocity QAEM 100 R/B
Average inclination QAEM 100 R/B
Mean right ascension of the ascending node (RAAN) QAEM 100 R/B
Mean argument of perigee QAEM 100 R/B
Mean semi-major axis of the orbit QAEM 100 R/B
Mean orbital eccentricity QAEM 100 R/B
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