OV1-5, 2122
Orbit data source: Space-Track
OV1-5, 2122 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Wed, 30 Mar 1966 UTC via an ATLAS 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.
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OV1-5 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 1 day ago |
| Origin | |
| Manufacturer | GD/Convair |
| Mission | Defense Early Warn/Tech |
| Bus & Motor | OV1, Unknown motor |
| Mass | 114 kg wet, 114 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Domed Cyl, 1.4 m |
| Radar Cross Section | 0.946 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 OV1-5
1 2122U 66025B 24276.28424553 .00000504 00000-0 29495-3 0 9991
2 2122 144.6335 156.5612 0047889 284.7263 74.8106 13.66051176920406Epoch: 2024-10-02T06:49Z
Definitive object data (Epoch: 2024-10-02T06:49:18.813Z)
| Latitude | -0.00002° |
| Longitude | 42.74701° |
| Altitude | 1,003.686 km |
| Speed | 7.356 km/s |
| True Right ascension | 10h 26m 14s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Predictive object data (real-time)
| Latitude | -19.07764° |
| Longitude | -160.00087° |
| Altitude | 1,010.566 km |
| Speed | 7.351 km/s |
| Apparent Right ascension | 20h 21m 07s |
| Apparent Declination | -28° 57' 41" |
| Sunlit | Object is in full shadow |
Predictive observer data (real-time)
| Local Sidereal Time | 07:32:16 |
| Azimuth | 313.772° NW |
| Elevation | -75.147° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 1,052.165 km |
| Perigee | 981.338 km |
| Semi-major axis | 7,394.888 km |
| Eccentricity | 0.0047889 |
| Inclination | 144.6335° |
| RAAN | 156.5612° |
| Arg. of periapsis | 284.7263° |
| True anomaly | 75.34102° |
| Mean anomaly | 74.8106° |
| Eccentric anomaly | 75.07573° |
| Mean motion | 3.41307 °/min |
| BSTAR | 0.00029495 |
| Period | 105.48 mins |
No data available
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Other satellites on launch #25 in the year 1966 (1966-03-30 UTC)
| OV1-4, 2121 |
| OV1-5, 2122 |
| OV1-5 R/B, 2123 |
| OV1-4 R/B, 2124 |
| OV1-5 DEB, 3611 (Decayed) |
| OV1-5 DEB, 5361 |
| OV1-5 DEB, 5599 |
| OV1-5 DEB, 27880 |
OV1-5 Visibility forecast
Observer location: 39.9160978°, -105.1181434
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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