OPS 0340, 2125
Orbit data source: Space-Track
OPS 0340, 2125 is a payload satellite owned by USAF SSD (US) in SSO that was launched on Thu, 31 Mar 1966 UTC via a THOR BURNER 1 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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2125 intel report (Beta)
OPS 0340 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 15 hours ago |
| Origin | |
| Manufacturer | RCA/East Windsor |
| Mission | Defense Weather |
| Bus & Motor | P35?, Unknown motor |
| Mass | 72 kg wet, 72 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl, 0.6 m |
| Radar Cross Section | 0.377 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 15 hours ago
0 OPS 0340
1 02125U 66026A 24355.89241612 .00001880 00000-0 34800-3 0 9997
2 02125 97.9903 171.0422 0150004 148.4215 212.6096 14.59457889 80263Epoch: 2024-12-20T21:25Z
Definitive object data (Epoch: 2024-12-20T21:25:04.752Z)
| Latitude | -0.00002° |
| Longitude | 119.821° |
| Altitude | 787.763 km |
| Speed | 7.412 km/s |
| True Right ascension | 11h 24m 10s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -32.26026° |
| Longitude | 125.46549° |
| Altitude | 813.165 km |
| Speed | 7.389 km/s |
| Apparent Right ascension | 14h 03m 54s |
| Apparent Declination | -79° 01' 29" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 11:06:12 |
| Azimuth | 170.987° S |
| Elevation | -31.712° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 798.051 km |
| Perigee altitude | 585.942 km |
| Semi-major axis | 7,070.133 km |
| Eccentricity | 0.0150004 |
| Inclination | 97.9903° |
| RAAN | 171.0422° |
| Arg. of periapsis | 148.4215° |
| True anomaly | 211.6977° |
| Mean anomaly | 212.6096° |
| Eccentric anomaly | 212.15222° |
| Mean motion | 3.65092 °/min |
| BSTAR | 0.000348 |
| Orbital period | 98.61 mins |
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Other satellites on launch #26 in the year 1966 (1966-03-31 UTC)
| OPS 0340, 2125 |
| THOR ALTAIR R/B, 2129 (Decayed) |
| THOR ALTAIR DEB, 2162 (Decayed) |
| THOR ALTAIR DEB, 2177 |
| THOR ALTAIR DEB, 2178 (Decayed) |
| THOR ALTAIR DEB, 2179 (Decayed) |
OPS 0340 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2024-12-21 12:20:27.813Z | 188.551° SSW | 2024-12-21 12:24:27.813Z | 256.07° W | 36.582° | 2024-12-21 12:28:27.813Z | 332.212° NNW |
| 6 mins | 2024-12-22 00:20:27.813Z | 37.501° NE | 2024-12-22 00:23:27.813Z | 116.182° SE | 32.049° | 2024-12-22 00:26:27.813Z | 167.03° S |
| 7 mins | 2024-12-22 11:24:27.813Z | 134.282° SE | 2024-12-22 11:27:27.813Z | 71.43° E | 34.854° | 2024-12-22 11:31:27.813Z | 2.97° NNE |
Authenticating...
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