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 25039.93725897 .00000984 00000-0 18663-3 0 9997
2 02125 97.9943 219.2832 0148838 352.4126 7.4822 14.59626359 87564Epoch: 2025-02-08T22:29Z
Definitive object data (Epoch: 2025-02-08T22:29:39.175Z)
| Latitude | -0.00004° |
| Longitude | 102.592° |
| Altitude | 593.008 km |
| Speed | 7.619 km/s |
| True Right ascension | 14h 37m 07s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 54.89999° |
| Longitude | -65.32593° |
| Altitude | 775.769 km |
| Speed | 7.433 km/s |
| Apparent Right ascension | 03h 50m 13s |
| Apparent Declination | 11° 05' 11" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 16:11:02 |
| Azimuth | 6.557° NNE |
| Elevation | -38.769° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 796.674 km |
| Perigee altitude | 586.23 km |
| Semi-major axis | 7,069.589 km |
| Eccentricity | 0.0148838 |
| Inclination | 97.9943° |
| RAAN | 219.2832° |
| Arg. of periapsis | 352.4126° |
| True anomaly | 7.70846° |
| Mean anomaly | 7.4822° |
| Eccentric anomaly | 7.59491° |
| Mean motion | 3.65134 °/min |
| BSTAR | 0.00018663 |
| Orbital period | 98.59 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 | 2025-02-09 23:44:52.849Z | 40.452° NE | 2025-02-09 23:48:52.849Z | 93.298° ESE | 23.084° | 2025-02-09 23:52:52.849Z | 147.191° SSE |
| 7 mins | 2025-02-10 01:23:52.849Z | 342.596° N | 2025-02-10 01:26:52.849Z | 280.691° WNW | 31.708° | 2025-02-10 01:30:52.849Z | 224.947° SW |
| 4 mins | 2025-02-10 10:51:52.849Z | 88.786° E | 2025-02-10 10:52:52.849Z | 70.527° E | 19.091° | 2025-02-10 10:55:52.849Z | 23.272° NE |
| 6 mins | 2025-02-10 12:27:52.849Z | 207.853° SW | 2025-02-10 12:30:52.849Z | 275.046° WNW | 28.692° | 2025-02-10 12:33:52.849Z | 324.559° NNW |
Authenticating...
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