OV3-3, 2389
Orbit data source: Space-Track
OV3-3, 2389 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Thu, 04 Aug 1966 UTC via an SCOUT B 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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2389 intel report (Beta)
OV3-3 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 18 hours ago |
| Origin | |
| Manufacturer | Space General |
| Mission | Civil Science |
| Bus & Motor | OV3, Unknown motor |
| Mass | 77 kg wet, 77 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Oct Cyl + 2 Rod, 1.5 m |
| Radar Cross Section | 0.548 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 18 hours ago
0 OV3-3
1 02389U 66070A 24355.84768152 .00016763 00000-0 80267-3 0 9990
2 02389 81.3313 84.4778 1082931 110.8266 261.2153 13.28864766526339Epoch: 2024-12-20T20:20Z
Definitive object data (Epoch: 2024-12-20T20:20:39.683Z)
| Latitude | -0.00008° |
| Longitude | 49.40513° |
| Altitude | 1,362.013 km |
| Speed | 7.078 km/s |
| True Right ascension | 05h 37m 54s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -75.82193° |
| Longitude | 11.84968° |
| Altitude | 1,984.962 km |
| Speed | 6.523 km/s |
| Apparent Right ascension | 01h 36m 27s |
| Apparent Declination | -61° 02' 41" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:59:03 |
| Azimuth | 192.175° SSW |
| Elevation | -68.1° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,963.339 km |
| Perigee altitude | 333.221 km |
| Semi-major axis | 7,526.417 km |
| Eccentricity | 0.1082931 |
| Inclination | 81.3313° |
| RAAN | 84.4778° |
| Arg. of periapsis | 110.8266° |
| True anomaly | 249.28649° |
| Mean anomaly | 261.2153° |
| Eccentric anomaly | 255.21597° |
| Mean motion | 3.324 °/min |
| BSTAR | 0.00080267 |
| Orbital period | 108.3 mins |
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Other satellites on launch #70 in the year 1966 (1966-08-04 UTC)
| OV3-3, 2389 |
| SCOUT B R/B, 2404 (Decayed) |
| SCOUT B DEB, 2521 (Decayed) |
| SCOUT B DEB, 2800 |
OV3-3 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2024-12-21 18:37:00.721Z | 307.709° NW | 2024-12-21 18:39:00.721Z | 249.045° W | 22.951° | 2024-12-21 18:41:00.721Z | 210.958° SW |
| 8 mins | 2024-12-22 06:48:00.721Z | 183.553° SSW | 2024-12-22 06:52:00.721Z | 157.792° S | 43.753° | 2024-12-22 06:56:00.721Z | 12.183° NNE |
Authenticating...
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