RAPTOR2
Satellite information RAPTOR2 - 2024-028E
| Spacetrack Directory Name | RAPTOR2 |
| Alternative name | 2024-028E |
| Follow RAPTOR2 | RAPTOR2 Tracker |
| Pass predictions RAPTOR2 | Pass predictions RAPTOR2 |
| Orbit launches |
2024-02-14 (2 years ago)
|
| Days in orbit | 927 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 992 km |
| Apogee | 1005 km |
| Orbit slope (inclination) | 39.99° |
| Laps per day | 14 |
| Height RAPTOR2 | 1000.92 km |
Additional information RAPTOR2
RAPTOR2, 58959 is a payload satellite owned by SDA (US) in LEO that was launched on Wed, 14 Feb 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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 RAPTOR2 Date of exalting 14.02.2024y. Average height of ISS RAPTOR2 hundred 1000.92 km. Average velocity RAPTOR2 is 26472.92 km/h. Inclination RAPTOR2 satellite 39.99°.TLE
Average velocity RAPTOR2
Average inclination RAPTOR2
Mean right ascension of the ascending node (RAAN) RAPTOR2
Mean argument of perigee RAPTOR2
Mean semi-major axis of the orbit RAPTOR2
Mean orbital eccentricity RAPTOR2
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