AURORA 1, 2876
Orbit data source: Space-Track
AURORA 1, 2876 is an American payload satellite in LEO that was launched on Thu, 29 Jun 1967 UTC via a THOR BURNER 2 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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2876 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 AURORA 1
1 02876U 67065B 25287.06453000 .00000001 00000-0 -20597-3 0 9997
2 02876 89.9903 313.4494 0070896 339.2891 20.5079 8.36560634369020
TLE epoch observation values (Epoch: 2025-10-14T01:32:55.392Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #65 in the year 1967 (1967-06-29 UTC)
AURORA 1 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. |
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39 mins | 2025-10-15 12:46:19.135Z | 5.214° NNE | 2025-10-15 13:06:19.135Z | 85.773° E | 39.816° | 2025-10-15 13:25:19.135Z | 160.196° S |
35 mins | 2025-10-15 15:39:19.135Z | 354.123° N | 2025-10-15 15:56:19.135Z | 290.902° WNW | 35.397° | 2025-10-15 16:14:19.135Z | 226.608° WSW |
28 mins | 2025-10-15 23:37:19.135Z | 108.783° ESE | 2025-10-15 23:50:19.135Z | 61.874° ENE | 26.899° | 2025-10-16 00:05:19.135Z | 9.183° NNE |
38 mins | 2025-10-16 02:20:19.135Z | 182.167° SSW | 2025-10-16 02:39:19.135Z | 281.241° WNW | 44.312° | 2025-10-16 02:58:19.135Z | 357.266° N |
21 mins | 2025-10-16 05:26:19.135Z | 270.693° WNW | 2025-10-16 05:35:19.135Z | 301.034° NW | 16.371° | 2025-10-16 05:47:19.135Z | 340.483° 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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