OPS 1427 (OV3-4), 2201
Orbit data source: Space-Track
OPS 1427 (OV3-4), 2201 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Fri, 10 Jun 1966 UTC via an SCOUT B launch vehicle from the Wallops Island (WLPIS). 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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2201 intel report (Beta)
OPS 1427 (OV3-4) details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 10 hours ago |
| Origin | |
| Manufacturer | Space General |
| Mission | Defense Technology |
| Bus & Motor | OV3, Unknown motor |
| Mass | 78 kg wet, 78 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Oct Cyl, 0.7 m |
| Radar Cross Section | 0.548 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 10 hours ago
0 OPS 1427 (OV3-4)
1 02201U 66052A 24356.83370358 .00000005 00000-0 29057-4 0 9993
2 02201 40.8940 175.5425 2235613 235.0525 101.9556 10.09946871142497Epoch: 2024-12-21T20:00Z
Definitive object data (Epoch: 2024-12-21T20:00:31.989Z)
| Latitude | -0° |
| Longitude | 144.53003° |
| Altitude | 3,473.867 km |
| Speed | 6.07 km/s |
| True Right ascension | 11h 42m 10s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 40.53903° |
| Longitude | -136.76723° |
| Altitude | 4,375.603 km |
| Speed | 5.486 km/s |
| Apparent Right ascension | 17h 06m 19s |
| Apparent Declination | 12° 30' 23" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 05:21:56 |
| Azimuth | 4.804° NNE |
| Elevation | -37.452° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 4,686.039 km |
| Perigee altitude | 642.888 km |
| Semi-major axis | 9,042.601 km |
| Eccentricity | 0.2235613 |
| Inclination | 40.894° |
| RAAN | 175.5425° |
| Arg. of periapsis | 235.0525° |
| True anomaly | 125.01233° |
| Mean anomaly | 101.9556° |
| Eccentric anomaly | 113.68571° |
| Mean motion | 2.52408 °/min |
| BSTAR | 0.000029057 |
| Orbital period | 142.63 mins |
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Other satellites on launch #52 in the year 1966 (1966-06-10 UTC)
| OPS 1427 (OV3-4), 2201 |
| SCOUT B R/B, 2206 |
| SCOUT B DEB, 2498 |
| SCOUT B DEB, 2516 |
| SCOUT B DEB, 28265 |
OPS 1427 (OV3-4) 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. |
|---|---|---|---|---|---|---|---|
| 42 mins | 2024-12-22 12:38:13.038Z | 181.888° SSW | 2024-12-22 12:57:13.038Z | 124.916° SE | 30.728° | 2024-12-22 13:20:13.038Z | 71.429° E |
| 51 mins | 2024-12-22 15:07:13.038Z | 227.921° WSW | 2024-12-22 15:32:13.038Z | 151.75° SSE | 43.804° | 2024-12-22 15:58:13.038Z | 72.115° E |
| 49 mins | 2024-12-22 17:43:13.038Z | 263.482° W | 2024-12-22 18:12:13.038Z | 4.254° NNE | 44.974° | 2024-12-22 18:32:13.038Z | 89.577° E |
| 39 mins | 2024-12-22 20:24:13.038Z | 286.018° WNW | 2024-12-22 20:50:13.038Z | 198.512° SSW | 44.223° | 2024-12-22 21:03:13.038Z | 124.553° SE |
| 24 mins | 2024-12-22 23:06:13.038Z | 286.592° WNW | 2024-12-22 23:21:13.038Z | 236.057° WSW | 27.851° | 2024-12-22 23:30:13.038Z | 181.14° SSW |
Authenticating...
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