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 26080.86661005 .00000121 00000-0 16800-3 0 9990
2 01420 89.8742 287.3001 0072292 325.4426 45.6412 13.51889723991655TLE epoch observation values (Epoch: 2026-03-21T20:47:55.108Z)
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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-03-22 12:51:28.754Z | 123.682° SE | 2026-03-22 12:56:28.754Z | 69.675° E | 22.616° | 2026-03-22 13:00:28.754Z | 27.891° NE |
| 10 mins | 2026-03-22 14:37:28.754Z | 203° SW | 2026-03-22 14:42:28.754Z | 286.464° WNW | 37.664° | 2026-03-22 14:47:28.754Z | 345.076° N |
| 11 mins | 2026-03-23 01:46:28.754Z | 9.727° NNE | 2026-03-23 01:51:28.754Z | 93.949° ESE | 43.34° | 2026-03-23 01:57:28.754Z | 173.465° S |
| 8 mins | 2026-03-23 03:33:28.754Z | 323.176° NNW | 2026-03-23 03:37:28.754Z | 282.939° WNW | 18.368° | 2026-03-23 03:41:28.754Z | 246.432° 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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