OPS 1509 (TRANSIT 10), 1864
Orbit data source: Space-Track
OPS 1509 (TRANSIT 10), 1864 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Wed, 22 Dec 1965 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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1864 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 OPS 1509 (TRANSIT 10)
1 01864U 65109A 26152.24712482 .00000201 00000-0 17759-3 0 9991
2 01864 89.0739 236.8939 0107434 262.6480 96.2468 13.79056904 33908TLE epoch observation values (Epoch: 2026-06-01T05:55:51.584Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #109 in the year 1965 (1965-12-22 UTC)
OPS 1509 (TRANSIT 10) 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-02 04:42:35.706Z | 115.762° SE | 2026-06-02 04:46:35.706Z | 73.591° E | 19.638° | 2026-06-02 04:50:35.706Z | 32.429° NE |
| 11 mins | 2026-06-02 06:25:35.706Z | 195.699° SSW | 2026-06-02 06:30:35.706Z | 284.804° WNW | 40.991° | 2026-06-02 06:36:35.706Z | 351.746° N |
| 11 mins | 2026-06-02 17:21:35.706Z | 14.869° NNE | 2026-06-02 17:26:35.706Z | 80.634° E | 37.36° | 2026-06-02 17:32:35.706Z | 160.637° S |
| 7 mins | 2026-06-02 19:07:35.706Z | 322.215° NNW | 2026-06-02 19:10:35.706Z | 285.874° WNW | 22.581° | 2026-06-02 19:14:35.706Z | 239.242° 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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