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). Payload-class satellites include a variety of spacecraft 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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2176 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OPS 0082 (TRANSIT 13)
1 2176U 66041A 26123.42819140 .00000209 00000-0 12379-3 0 9992
2 2176 90.2288 82.0768 0059445 250.5752 108.8999 14.04313525 61156TLE epoch observation values (Epoch: 2026-05-03T10:16:35.736Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #41 in the year 1966 (1966-05-19 UTC)
OPS 0082 (TRANSIT 13) Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-05-03 20:39:48.502Z | 131.638° SE | 2026-05-03 20:43:48.502Z | 82.694° E | 26.28° | 2026-05-03 20:48:48.502Z | 20.644° NNE |
| 8 mins | 2026-05-03 22:22:48.502Z | 218.861° SW | 2026-05-03 22:25:48.502Z | 263.264° W | 30.689° | 2026-05-03 22:30:48.502Z | 336.214° NNW |
| 9 mins | 2026-05-04 09:06:48.502Z | 20.132° NNE | 2026-05-04 09:10:48.502Z | 90.441° ESE | 37.356° | 2026-05-04 09:15:48.502Z | 162.008° S |
| 7 mins | 2026-05-04 10:49:48.502Z | 321.775° NNW | 2026-05-04 10:52:48.502Z | 283.517° WNW | 20.128° | 2026-05-04 10:56:48.502Z | 238.394° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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