MIDAS 7/ERS 10, 622
Orbit data source: Space-Track
MIDAS 7/ERS 10, 622 is a payload satellite owned by USAF SSD (US) in LEO that was launched on Fri, 19 Jul 1963 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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Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 MIDAS 7/ERS 10
1 00622U 63030A 25259.35451485 .00000000 00000-0 -10687-2 0 9995
2 00622 88.4216 226.3138 0031354 334.5969 25.3339 8.57932472436297
TLE epoch observation values (Epoch: 2025-09-16T08:30:30.083Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #30 in the year 1963 (1963-07-19 UTC)
MIDAS 7/ERS 10 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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35 mins | 2025-09-17 23:43:03.864Z | 214.164° SW | 2025-09-18 00:00:03.864Z | 281.01° WNW | 35.054° | 2025-09-18 00:18:03.864Z | 353.94° N |
8 mins | 2025-09-18 06:11:03.864Z | 35.027° NE | 2025-09-18 06:14:03.864Z | 44.808° NE | 11.001° | 2025-09-18 06:19:03.864Z | 61.025° ENE |
36 mins | 2025-09-18 08:52:03.864Z | 4.198° NNE | 2025-09-18 09:10:03.864Z | 84.63° E | 41.012° | 2025-09-18 09:28:03.864Z | 161.49° S |
31 mins | 2025-09-18 11:41:03.864Z | 349.428° N | 2025-09-18 11:56:03.864Z | 290.636° WNW | 33.513° | 2025-09-18 12:12:03.864Z | 229.499° WSW |
25 mins | 2025-09-18 19:27:03.864Z | 102.451° ESE | 2025-09-18 19:39:03.864Z | 59.009° ENE | 23.102° | 2025-09-18 19:52:03.864Z | 13.626° NNE |
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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