OPS 1527 (OV3-1), 2150
Orbit data source: Space-Track
OPS 1527 (OV3-1), 2150 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Fri, 22 Apr 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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2150 intel report (Beta)
OPS 1527 (OV3-1) details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 16 hours ago |
| Origin | |
| Manufacturer | Space General |
| Mission | Civil Science |
| Bus & Motor | OV3, Unknown motor |
| Mass | 69 kg wet, 69 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Oct Cyl, 0.74 m |
| Radar Cross Section | 0.613 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 16 hours ago
0 OPS 1527 (OV3-1)
1 2150U 66034A 25023.08367835 .00028704 00000-0 15667-2 0 9997
2 2150 82.3702 161.1637 1455788 129.5392 244.3761 12.47732379337843Epoch: 2025-01-23T02:00Z
Definitive object data (Epoch: 2025-01-23T02:00:29.809Z)
| Latitude | -0.00006° |
| Longitude | 8.3732° |
| Altitude | 2,093.633 km |
| Speed | 6.586 km/s |
| True Right ascension | 10h 44m 39s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 75.47107° |
| Longitude | 157.0049° |
| Altitude | 427.849 km |
| Speed | 8.163 km/s |
| Apparent Right ascension | 06h 22m 08s |
| Apparent Declination | 36° 22' 39" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 19:07:32 |
| Azimuth | 9.359° NNE |
| Elevation | -12.995° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 2,613.962 km |
| Perigee altitude | 328.551 km |
| Semi-major axis | 7,849.394 km |
| Eccentricity | 0.1455788 |
| Inclination | 82.3702° |
| RAAN | 161.1637° |
| Arg. of periapsis | 129.5392° |
| True anomaly | 230.56811° |
| Mean anomaly | 244.3761° |
| Eccentric anomaly | 237.35286° |
| Mean motion | 3.12097 °/min |
| BSTAR | 0.0015667 |
| Orbital period | 115.35 mins |
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Other satellites on launch #34 in the year 1966 (1966-04-22 UTC)
| OPS 1527 (OV3-1), 2150 |
| SCOUT B R/B, 2167 (Decayed) |
| SCOUT B DEB, 2208 (Decayed) |
| SCOUT B DEB, 2209 (Decayed) |
OPS 1527 (OV3-1) 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-01-24 08:53:43.862Z | 156.964° SSE | 2025-01-24 09:00:43.862Z | 104.288° ESE | 33.661° | 2025-01-24 09:06:43.862Z | 27.128° NE |
| 11 mins | 2025-01-24 10:50:43.862Z | 224.145° SW | 2025-01-24 10:57:43.862Z | 284.01° WNW | 27.97° | 2025-01-24 11:01:43.862Z | 334.902° NNW |
Authenticating...
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