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 25260.16034985 .00000003 00000-0 78421-3 0 9996
2 02876 89.9982 313.4583 0070998 4.8298 355.3211 8.36560585366776
TLE epoch observation values (Epoch: 2025-09-17T03:50:54.227Z)
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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19 mins | 2025-09-18 12:16:30.725Z | 23.613° NE | 2025-09-18 12:26:30.725Z | 55.59° ENE | 13.937° | 2025-09-18 12:35:30.725Z | 84.055° E |
38 mins | 2025-09-18 15:05:30.725Z | 4.79° NNE | 2025-09-18 15:23:30.725Z | 82.08° E | 43.306° | 2025-09-18 15:43:30.725Z | 172.53° S |
31 mins | 2025-09-18 17:57:30.725Z | 351.33° N | 2025-09-18 18:12:30.725Z | 297.986° NW | 29.919° | 2025-09-18 18:28:30.725Z | 241.435° WSW |
31 mins | 2025-09-19 01:52:30.725Z | 123.281° SE | 2025-09-19 02:07:30.725Z | 64.555° ENE | 32.541° | 2025-09-19 02:23:30.725Z | 6.591° NNE |
37 mins | 2025-09-19 04:39:30.725Z | 195.835° SSW | 2025-09-19 04:56:30.725Z | 270.325° WNW | 41.547° | 2025-09-19 05:16:30.725Z | 355.778° 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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