OPS 8464 (TRANSIT 5B-7), 1514
Orbit data source: Space-Track
OPS 8464 (TRANSIT 5B-7), 1514 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Fri, 13 Aug 1965 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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1514 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 8464 (TRANSIT 5B-7)
1 01514U 65065F 25300.88055543 .00000141 00000-0 25616-3 0 9990
2 01514 89.9837 228.1238 0072039 94.6709 337.0428 13.35323612930265TLE epoch observation values (Epoch: 2025-10-27T21:07:59.989Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #65 in the year 1965 (1965-08-13 UTC)
OPS 8464 (TRANSIT 5B-7) 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 | 2025-10-28 06:23:06.235Z | 33.569° NE | 2025-10-28 06:28:06.235Z | 87.394° E | 21.76° | 2025-10-28 06:32:06.235Z | 127.671° SE |
| 10 mins | 2025-10-28 08:11:06.235Z | 346.725° N | 2025-10-28 08:15:06.235Z | 292.791° NW | 38.686° | 2025-10-28 08:21:06.235Z | 205.535° SW |
| 9 mins | 2025-10-28 18:30:06.235Z | 121.368° SE | 2025-10-28 18:34:06.235Z | 75.423° E | 24.812° | 2025-10-28 18:39:06.235Z | 23.078° NE |
| 11 mins | 2025-10-28 20:16:06.235Z | 203.836° SW | 2025-10-28 20:21:06.235Z | 265.416° W | 36.254° | 2025-10-28 20:27:06.235Z | 343.845° N |
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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