OPS 0082 (TRANSIT 13), 2176
Orbit data source: Space-Track
OPS 0082 (TRANSIT 13), 2176 is a payload satellite owned by USN NAVAIR (US) in LEO that was launched on Thu, 19 May 1966 UTC via an SCOUT A 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 0082 (TRANSIT 13) details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 13 hours ago |
| Origin | |
| Manufacturer | APL |
| Mission | Defense Navigation |
| Bus & Motor | TRANSIT 5, Unknown motor |
| Mass | 51 kg wet, 51 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Oct Cyl + 4 Pan + 1 Rod, Unknown HBR |
| Radar Cross Section | 7.565 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 13 hours ago
0 OPS 0082 (TRANSIT 13)
1 02176U 66041A 24284.46539873 .00001558 00000-0 96546-3 0 9990
2 02176 90.2208 67.7284 0065182 252.8568 106.5469 14.03819389981185Epoch: 2024-10-10T11:10Z
Definitive object data (Epoch: 2024-10-10T11:10:10.45Z)
| Latitude | 0° |
| Longitude | -119.3647° |
| Altitude | 897.391 km |
| Speed | 7.396 km/s |
| True Right ascension | 04h 30m 54s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Predictive object data (real-time)
| Latitude | -78.80542° |
| Longitude | -118.2413° |
| Altitude | 867.64 km |
| Speed | 7.439 km/s |
| Apparent Right ascension | 06h 19m 44s |
| Apparent Declination | -61° 13' 44" |
| Sunlit | Object is in daylight |
Predictive observer data (real-time)
| Local Sidereal Time | 18:48:50 |
| Azimuth | 170.545° S |
| Elevation | -68.224° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 924.865 km |
| Perigee | 830.277 km |
| Semi-major axis | 7,255.708 km |
| Eccentricity | 0.0065182 |
| Inclination | 90.2208° |
| RAAN | 67.7284° |
| Arg. of periapsis | 252.8568° |
| True anomaly | 107.26122° |
| Mean anomaly | 106.5469° |
| Eccentric anomaly | 106.90423° |
| Mean motion | 3.51175 °/min |
| BSTAR | 0.00096546 |
| Period | 102.51 mins |
No data available
No data available
Other satellites on launch #41 in the year 1966 (1966-05-19 UTC)
| OPS 0082 (TRANSIT 13), 2176 |
| SCOUT A R/B, 2180 |
| SCOUT A DEB, 2225 (Decayed) |
| SCOUT A DEB, 2644 |
| SCOUT A DEB, 3591 |
| SCOUT A DEB, 4555 |
| SCOUT A DEB, 28210 (Decayed) |
| SCOUT A DEB, 31407 |
| TRANSIT 13 DEB, 42667 (Decayed) |
OPS 0082 (TRANSIT 13) 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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