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: 8 hours ago
TLE from 8 hours ago
0 OPS 6582 (TRANSIT 5B-5)
1 00965U 64083D 25310.20132873 .00000109 00000-0 13912-3 0 9997
2 00965 90.0705 201.3337 0040395 207.8151 272.2349 13.56984890 13373TLE epoch observation values (Epoch: 2025-11-06T04:49:54.802Z)
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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-06 16:44:19.234Z | 153.466° SSE | 2025-11-06 16:49:19.234Z | 95.575° ESE | 38.324° | 2025-11-06 16:55:19.234Z | 9.639° NNE |
| 8 mins | 2025-11-06 18:32:19.234Z | 237.335° WSW | 2025-11-06 18:36:19.234Z | 283.652° WNW | 22.467° | 2025-11-06 18:40:19.234Z | 325.839° NNW |
| 7 mins | 2025-11-07 03:53:19.234Z | 49.085° ENE | 2025-11-07 03:56:19.234Z | 83.517° E | 19.052° | 2025-11-07 04:00:19.234Z | 123.699° SE |
| 11 mins | 2025-11-07 05:37:19.234Z | 352.157° N | 2025-11-07 05:42:19.234Z | 278.976° WNW | 41.051° | 2025-11-07 05:48:19.234Z | 199.554° SSW |
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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