ESSA 2 (OT-2), 2091
Orbit data source: Space-Track
ESSA 2 (OT-2), 2091 is a payload satellite owned by ESSA (US) in SSO that was launched on Mon, 28 Feb 1966 UTC via a THOR DELTA E launch vehicle from the Air Force Eastern Test Range (AFETR). 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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2091 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ESSA 2 (OT-2)
1 02091U 66016A 25292.26836840 -.00000019 00000-0 12397-3 0 9994
2 02091 101.2357 202.3877 0039146 25.9137 94.9028 12.69425630763053
TLE epoch observation values (Epoch: 2025-10-19T06:26:27.029Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)
ESSA 2 (OT-2) 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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14 mins | 2025-10-19 17:16:30.012Z | 138.083° SSE | 2025-10-19 17:22:30.012Z | 77.578° E | 39.133° | 2025-10-19 17:30:30.012Z | 351.838° N |
11 mins | 2025-10-19 19:09:30.012Z | 212.237° SW | 2025-10-19 19:14:30.012Z | 261.458° W | 26.956° | 2025-10-19 19:20:30.012Z | 318.743° NNW |
6 mins | 2025-10-20 05:12:30.012Z | 68.802° E | 2025-10-20 05:15:30.012Z | 92.708° ESE | 13.828° | 2025-10-20 05:18:30.012Z | 115.706° SE |
14 mins | 2025-10-20 07:01:30.012Z | 20.073° NNE | 2025-10-20 07:07:30.012Z | 96.032° ESE | 44.642° | 2025-10-20 07:15:30.012Z | 194.321° SSW |
10 mins | 2025-10-20 08:53:30.012Z | 346.084° N | 2025-10-20 08:58:30.012Z | 301.802° NW | 21.339° | 2025-10-20 09:03:30.012Z | 260.677° W |
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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