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: 18 hours ago
TLE from 18 hours ago
0 OPS 8464 (TRANSIT 5B-7)
1 01514U 65065F 25344.43716544 .00000128 00000-0 23359-3 0 9991
2 01514 89.9852 228.0658 0069774 333.7746 199.8886 13.35334683936074TLE epoch observation values (Epoch: 2025-12-10T10:29:31.094Z)
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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-12-11 06:00:50.393Z | 334.176° NNW | 2025-12-11 06:05:50.393Z | 282.446° WNW | 24.669° | 2025-12-11 06:10:50.393Z | 233.994° WSW |
| 11 mins | 2025-12-11 16:18:50.393Z | 154.912° SSE | 2025-12-11 16:23:50.393Z | 76.197° E | 40.363° | 2025-12-11 16:29:50.393Z | 6.81° NNE |
| 9 mins | 2025-12-11 18:07:50.393Z | 239.096° WSW | 2025-12-11 18:11:50.393Z | 281.685° WNW | 20.997° | 2025-12-11 18:16:50.393Z | 329.647° NNW |
| 10 mins | 2025-12-12 03:36:50.393Z | 34.343° NE | 2025-12-12 03:40:50.393Z | 80.033° E | 26.894° | 2025-12-12 03:46:50.393Z | 140.512° SSE |
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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