OV3-3, 2389
Orbit data source: Space-Track
OV3-3, 2389 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Thu, 04 Aug 1966 UTC via an SCOUT B 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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2389 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 OV3-3
1 02389U 66070A 26110.54562939 .00008746 00000-0 39766-3 0 9993
2 02389 81.3308 21.8302 1015669 307.2098 44.0441 13.44238714591223TLE epoch observation values (Epoch: 2026-04-20T13:05:42.379Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #70 in the year 1966 (1966-08-04 UTC)
OV3-3 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-04-20 20:22:53.953Z | 250.841° W | 2026-04-20 20:27:53.953Z | 304.034° NW | 21.217° | 2026-04-20 20:32:53.953Z | 344.942° N |
| 14 mins | 2026-04-21 03:58:53.953Z | 17.507° NNE | 2026-04-21 04:05:53.953Z | 63.395° ENE | 22.984° | 2026-04-21 04:12:53.953Z | 108.848° ESE |
| 19 mins | 2026-04-21 05:45:53.953Z | 351.614° N | 2026-04-21 05:54:53.953Z | 19.095° NNE | 44.826° | 2026-04-21 06:04:53.953Z | 171.97° S |
| 14 mins | 2026-04-21 07:35:53.953Z | 322.379° NNW | 2026-04-21 07:41:53.953Z | 283.93° WNW | 23.258° | 2026-04-21 07:49:53.953Z | 232.06° WSW |
| 10 mins | 2026-04-21 17:47:53.953Z | 135.129° SSE | 2026-04-21 17:51:53.953Z | 83.099° E | 27.661° | 2026-04-21 17:57:53.953Z | 28.058° NE |
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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