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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OPS 0340 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 12 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 12 hours ago
0 OPS 0340
1 02125U 66026A 24278.47787210 .00003230 00000-0 59548-3 0 9991
2 02125 97.9920 96.4546 0150982 31.8142 329.2070 14.59051393 68979Epoch: 2024-10-04T11:28Z
Definitive object data (Epoch: 2024-10-04T11:28:08.149Z)
| Latitude | -0.00004° |
| Longitude | -89.22731° |
| Altitude | 607.889 km |
| Speed | 7.604 km/s |
| True Right ascension | 06h 25m 49s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Predictive object data (real-time)
| Latitude | 62.01205° |
| Longitude | -103.98692° |
| Altitude | 616.5 km |
| Speed | 7.605 km/s |
| Apparent Right ascension | 05h 18m 03s |
| Apparent Declination | 14° 16' 34" |
| Sunlit | Object is in daylight |
Predictive observer data (real-time)
| Local Sidereal Time | 17:12:12 |
| Azimuth | 358.251° N |
| Elevation | -35.791° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 800.077 km |
| Perigee | 586.544 km |
| Semi-major axis | 7,071.448 km |
| Eccentricity | 0.0150982 |
| Inclination | 97.992° |
| RAAN | 96.4546° |
| Arg. of periapsis | 31.8142° |
| True anomaly | 328.30673° |
| Mean anomaly | 329.207° |
| Eccentric anomaly | 328.75834° |
| Mean motion | 3.6499 °/min |
| BSTAR | 0.00059548 |
| Period | 98.63 mins |
No data available
No data available
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: 39.9160978°, -105.1181434
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. |
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