ESSA 5, 2757
Orbit data source: Space-Track
ESSA 5, 2757 is a payload satellite owned by ESSA (US) in SSO that was launched on Thu, 20 Apr 1967 UTC via a THOR DELTA E 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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2757 intel report (Beta)
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TLE from 8 hours ago
0 ESSA 5
1 2757U 67036A 25201.07794286 -.00000027 00000-0 10655-3 0 9996
2 2757 101.9673 6.1275 0042824 183.6127 288.6786 12.68536608697304
TLE epoch observation values (Epoch: 2025-07-20T01:52:14.263Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #36 in the year 1967 (1967-04-20 UTC)
ESSA 5 Visibility forecast
Observer location: undefined°, undefined°
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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15 mins | 2025-07-20 10:49:45.725Z | 163.148° S | 2025-07-20 10:57:45.725Z | 283.91° WNW | 44.796° | 2025-07-20 11:04:45.725Z | 340.768° N |
7 mins | 2025-07-20 12:46:45.725Z | 243.714° WSW | 2025-07-20 12:49:45.725Z | 267.447° W | 14.941° | 2025-07-20 12:53:45.725Z | 298.771° NW |
11 mins | 2025-07-20 22:45:45.725Z | 46.624° ENE | 2025-07-20 22:50:45.725Z | 92.356° ESE | 24.637° | 2025-07-20 22:56:45.725Z | 147.849° SSE |
13 mins | 2025-07-21 00:36:45.725Z | 8.13° NNE | 2025-07-21 00:42:45.725Z | 298.988° NW | 41.265° | 2025-07-21 00:49:45.725Z | 217.442° SW |
5 mins | 2025-07-21 02:30:45.725Z | 329.764° NNW | 2025-07-21 02:32:45.725Z | 313.885° NW | 12.956° | 2025-07-21 02:35:45.725Z | 290.658° WNW |
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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