LEMUR 2 MJR092620
Satellite information LEMUR 2 MJR092620 - 2023-174CN
| Spacetrack Directory Name | LEMUR 2 MJR092620 |
| Alternative name | 2023-174CN |
| Follow LEMUR 2 MJR092620 | LEMUR 2 MJR092620 Tracker |
| Pass predictions LEMUR 2 MJR092620 | Pass predictions LEMUR 2 MJR092620 |
| Orbit launches |
2023-11-11 g.01:00 (2 years ago)
|
| Days in orbit | 1063 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 512 km |
| Apogee | 527 km |
| Orbit slope (inclination) | 97.4° |
| Laps per day | 15 |
| Height LEMUR 2 MJR092620 | 449.33 km |
Additional information LEMUR 2 MJR092620
LEMUR 2 MJR092620, 58340 is an American payload satellite in SSO that was launched on Sat, 11 Nov 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite LEMUR 2 MJR092620 Date of exalting 11.11.2023y. Average height of ISS LEMUR 2 MJR092620 hundred 449.33 km. Average velocity LEMUR 2 MJR092620 is 27518.86 km/h. Inclination LEMUR 2 MJR092620 satellite 97.4°.TLE
Average velocity LEMUR 2 MJR092620
Average inclination LEMUR 2 MJR092620
Mean right ascension of the ascending node (RAAN) LEMUR 2 MJR092620
Mean argument of perigee LEMUR 2 MJR092620
Mean semi-major axis of the orbit LEMUR 2 MJR092620
Mean orbital eccentricity LEMUR 2 MJR092620
Frequency LEMUR 2 MJR092620
In the table below we show the frequencies LEMUR 2 MJR092620.
| Downlink |
|---|
| 401.100 MHz |
ISS
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