MIDAS 3, 163
Orbit data source: Space-Track
MIDAS 3, 163 is a payload satellite owned by USAF SSD (US) in LEO that was launched on Wed, 12 Jul 1961 UTC via an ATLAS AGENA B 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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163 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 MIDAS 3
1 00163U 61018A 25260.18505934 .00000005 00000-0 13033-2 0 9993
2 00163 91.1088 193.5088 0100877 94.5493 266.6910 8.91838240 89673
TLE epoch observation values (Epoch: 2025-09-17T04:26:29.126Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #18 in the year 1961 (1961-07-12 UTC)
MIDAS 3 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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33 mins | 2025-09-18 08:07:07.593Z | 1.56° NNE | 2025-09-18 08:23:07.593Z | 291.934° WNW | 44.679° | 2025-09-18 08:40:07.593Z | 194.412° SSW |
20 mins | 2025-09-18 10:50:07.593Z | 344.107° N | 2025-09-18 11:00:07.593Z | 305.423° NW | 19.659° | 2025-09-18 11:10:07.593Z | 267.723° W |
29 mins | 2025-09-18 18:13:07.593Z | 131.591° SE | 2025-09-18 18:27:07.593Z | 70.555° E | 35.293° | 2025-09-18 18:42:07.593Z | 5.287° NNE |
32 mins | 2025-09-18 20:51:07.593Z | 200.294° SSW | 2025-09-18 21:07:07.593Z | 276.299° WNW | 39.278° | 2025-09-18 21:23:07.593Z | 350.762° N |
25 mins | 2025-09-19 05:41:07.593Z | 17.251° NNE | 2025-09-19 05:55:07.593Z | 76.112° E | 27.624° | 2025-09-19 06:06:07.593Z | 124.388° SE |
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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