OPS 8480 (TRANSIT 5B-6), 1420
Orbit data source: Space-Track
OPS 8480 (TRANSIT 5B-6), 1420 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Thu, 24 Jun 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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1420 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 OPS 8480 (TRANSIT 5B-6)
1 01420U 65048A 26260.05741667 .00000069 00000-0 87669-4 0 9997
2 01420 89.8710 285.0453 0074053 163.1746 225.5396 13.51921170 15879TLE epoch observation values (Epoch: 2026-09-17T01:22:40.800Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #48 in the year 1965 (1965-06-24 UTC)
OPS 8480 (TRANSIT 5B-6) 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-18 00:30:09.386Z | 96.132° ESE | 2026-09-18 00:33:09.386Z | 67.058° ENE | 15.69° | 2026-09-18 00:36:09.386Z | 39.294° NE |
| 11 mins | 2026-09-18 02:13:09.386Z | 180.331° SSW | 2026-09-18 02:18:09.386Z | 246.305° WSW | 82.525° | 2026-09-18 02:24:09.386Z | 355.96° N |
| 10 mins | 2026-09-18 13:23:09.386Z | 25.037° NE | 2026-09-18 13:27:09.386Z | 82.479° E | 41.621° | 2026-09-18 13:33:09.386Z | 155.46° SSE |
| 9 mins | 2026-09-18 15:09:09.386Z | 333.847° NNW | 2026-09-18 15:13:09.386Z | 287.287° WNW | 28.701° | 2026-09-18 15:18:09.386Z | 229.477° 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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