OPS 6582 (TRANSIT 5B-5), 965
Orbit data source: Space-Track
OPS 6582 (TRANSIT 5B-5), 965 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Sun, 13 Dec 1964 UTC via a THOR ABLESTAR 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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965 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 OPS 6582 (TRANSIT 5B-5)
1 00965U 64083D 25362.83737478 .00000065 00000-0 77576-4 0 9993
2 00965 90.0663 201.7123 0043130 57.5510 4.0805 13.56992945 20514TLE epoch observation values (Epoch: 2025-12-28T20:05:49.180Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #83 in the year 1964 (1964-12-13 UTC)
OPS 6582 (TRANSIT 5B-5) 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-12-29 13:35:02.267Z | 167.618° S | 2025-12-29 13:41:02.267Z | 105.779° ESE | 43.473° | 2025-12-29 13:47:02.267Z | 2.525° NNE |
| 5 mins | 2025-12-29 15:26:02.267Z | 262.594° W | 2025-12-29 15:28:02.267Z | 284.245° WNW | 15.599° | 2025-12-29 15:31:02.267Z | 314.483° NW |
| 9 mins | 2025-12-30 00:44:02.267Z | 37.769° NE | 2025-12-30 00:48:02.267Z | 90.029° ESE | 25.392° | 2025-12-30 00:53:02.267Z | 140.618° SSE |
| 10 mins | 2025-12-30 02:29:02.267Z | 343.052° N | 2025-12-30 02:34:02.267Z | 269.581° W | 34.378° | 2025-12-30 02:39:02.267Z | 213.047° SW |
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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