QAEM 100 R/B
Satellite information QAEM 100 R/B
| Spacetrack Directory Name | QAEM 100 R/B |
| Follow QAEM 100 R/B | QAEM 100 R/B Tracker |
| Pass predictions QAEM 100 R/B | Pass predictions QAEM 100 R/B |
| Orbit launches |
2024-01-20 (2 years ago)
|
| Days in orbit | 945 |
| Country/organisation of origin | Iran (IRAN) |
| Starting point | SMTS (Shahrud Missile Test Site) |
| WWW | Here |
| Perigee | 724 km |
| Apogee | 768 km |
| Orbit slope (inclination) | 64.5° |
| Laps per day | 14 |
| Height QAEM 100 R/B | 753.75 km |
Additional information QAEM 100 R/B
QAEM 100 R/B, 58818 is space debris in LEO originally from a launch on Sat, 20 Jan 2024 UTC launched 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 20.01.2024y. Average height of ISS QAEM 100 R/B hundred 753.75 km. Average velocity QAEM 100 R/B is 26926 km/h. Inclination QAEM 100 R/B satellite 64.5°.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
Frequency QAEM 100 R/B
In the table below we show the frequencies QAEM 100 R/B.
| Downlink | Mode |
|---|---|
| 435.000 MHz | FSK |
| 437.540 MHz | FSK |
ISS
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