OV2-5, 3428
Orbit data source: Space-Track
OV2-5, 3428 is a payload satellite owned by SAMSO (US) that was launched on Thu, 26 Sep 1968 UTC via a TITAN IIIC 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.
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3428 intel report (Beta)
OV2-5 details
Identifier | |
Orbit | Active |
Last TLE update | 14 hours ago |
Origin | |
Manufacturer | Northrop |
Mission | Non-operational Civil Science |
Bus & Motor | OV2, Unknown motor |
Mass | ~200 kg wet, ~200 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Box + 4 Pan, 2.5 m |
Radar Cross Section | 1.167 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 14 hours ago
0 OV2-5
1 03428U 68081A 24325.69184463 .00000055 00000-0 00000-0 0 9997
2 03428 1.0960 14.8335 0080827 307.3946 184.5082 1.01557163115235
Epoch: 2024-11-20T16:36Z
Definitive object data (Epoch: 2024-11-20T16:36:15.376Z)
Latitude | 0.81099° |
Longitude | -162.59392° |
Altitude | 35,764.937 km |
Speed | 3.063 km/s |
True Right ascension | 09h 46m 37s |
True Declination | 0° 48' 37" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -0.32471° |
Longitude | 47.59744° |
Altitude | 35,151.813 km |
Speed | 3.108 km/s |
Apparent Right ascension | 23h 23m 54s |
Apparent Declination | -6° 19' 17" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 03:24:18 |
Azimuth | 244.968° WSW |
Elevation | 18.021° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 35,769.073 km |
Perigee altitude | 35,093.21 km |
Semi-major axis | 41,809.278 km |
Eccentricity | 0.0080827 |
Inclination | 1.096° |
RAAN | 14.8335° |
Arg. of periapsis | 307.3946° |
True anomaly | 184.43612° |
Mean anomaly | 184.5082° |
Eccentric anomaly | 184.47209° |
Mean motion | 0.25388 °/min |
BSTAR | Unknown |
Orbital period | 1417.97 mins |
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Other satellites on launch #81 in the year 1968 (1968-09-26 UTC)
OV2-5 Visibility forecast
Observer location: undefined°, undefined
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. |
---|---|---|---|---|---|---|---|
1440 mins | 2024-11-21 06:21:46.807Z | 244.953° WSW | 2024-11-22 06:21:46.807Z | 241.146° WSW | 20.12° | 2024-11-22 06:21:46.807Z | 241.146° WSW |
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