TEMPSAT 2
Satellite information TEMPSAT 2
| Spacetrack Directory Name | TEMPSAT 2 |
| Follow TEMPSAT 2 | TEMPSAT 2 Tracker |
| Pass predictions TEMPSAT 2 | Pass predictions TEMPSAT 2 |
| Orbit launches |
1969-09-30 (56 years ago)
|
| Days in orbit | 20791 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 893 km |
| Apogee | 925 km |
| Orbit slope (inclination) | 70.01° |
| Laps per day | 14 |
| Height TEMPSAT 2 | 918.04 km |
Additional information TEMPSAT 2
TEMPSAT 2, 4168 is a payload satellite owned by NRL (US) in LEO that was launched on Tue, 30 Sep 1969 UTC via a THORAD SLV-2G AGENA D 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 TEMPSAT 2 Date of exalting 30.09.1969y. Average height of ISS TEMPSAT 2 hundred 918.04 km. Average velocity TEMPSAT 2 is 26620.61 km/h. Inclination TEMPSAT 2 satellite 70.02°.TLE
Average velocity TEMPSAT 2
Average inclination TEMPSAT 2
Mean right ascension of the ascending node (RAAN) TEMPSAT 2
Mean argument of perigee TEMPSAT 2
Mean semi-major axis of the orbit TEMPSAT 2
Mean orbital eccentricity TEMPSAT 2
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