STEP 2
Satellite information STEP 2
| Spacetrack Directory Name | STEP 2 |
| Follow STEP 2 | STEP 2 Tracker |
| Pass predictions STEP 2 | Pass predictions STEP 2 |
| Orbit launches |
1994-05-19 (32 years ago)
|
| Days in orbit | 11788 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 568 km |
| Apogee | 716 km |
| Orbit slope (inclination) | 81.94° |
| Laps per day | 15 |
| Height STEP 2 | 607.16 km |
Additional information STEP 2
STEP 2, 23105 is a payload satellite owned by USAF STP (US) in LEO that was launched on Thu, 19 May 1994 UTC via a PEGASUS/HAPS 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 STEP 2 Date of exalting 19.05.1994y. Average height of ISS STEP 2 hundred 607.16 km. Average velocity STEP 2 is 27206.06 km/h. Inclination STEP 2 satellite 81.94°.TLE
Average velocity STEP 2
Average inclination STEP 2
Mean right ascension of the ascending node (RAAN) STEP 2
Mean argument of perigee STEP 2
Mean semi-major axis of the orbit STEP 2
Mean orbital eccentricity STEP 2
ISS
Buy us a coffee!
