SECOR 4 (EGRS 4)
Satellite information SECOR 4 (EGRS 4)
| Spacetrack Directory Name | SECOR 4 (EGRS 4) |
| Follow SECOR 4 (EGRS 4) | SECOR 4 (EGRS 4) Tracker |
| Pass predictions SECOR 4 (EGRS 4) | Pass predictions SECOR 4 (EGRS 4) |
| Orbit launches |
1965-04-03 g.01:00 (61 years ago)
|
| Days in orbit | 22435 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | Here |
| Perigee | 1267 km |
| Apogee | 1316 km |
| Orbit slope (inclination) | 90.26° |
| Laps per day | 13 |
| Height SECOR 4 (EGRS 4) | 1303.14 km |
Additional information SECOR 4 (EGRS 4)
SECOR 4 (EGRS 4), 1315 is an American payload satellite in LEO that was launched on Sat, 03 Apr 1965 UTC via an ATLAS SLV-3 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 SECOR 4 (EGRS 4) Date of exalting 03.04.1965y. Average height of ISS SECOR 4 (EGRS 4) hundred 1303.14 km. Average velocity SECOR 4 (EGRS 4) is 25943.98 km/h. Inclination SECOR 4 (EGRS 4) satellite 90.25°.TLE
Average velocity SECOR 4 (EGRS 4)
Average inclination SECOR 4 (EGRS 4)
Mean right ascension of the ascending node (RAAN) SECOR 4 (EGRS 4)
Mean argument of perigee SECOR 4 (EGRS 4)
Mean semi-major axis of the orbit SECOR 4 (EGRS 4)
Mean orbital eccentricity SECOR 4 (EGRS 4)
Frequency SECOR 4 (EGRS 4)
In the table below we show the frequencies SECOR 4 (EGRS 4).
| Downlink | Mode |
|---|---|
| 136.845 MHz | FM |
ISS
Buy us a coffee!
