ERS 9, 635
Orbit data source: Space-Track
ERS 9, 635 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: 3 months ago
TLE from 3 months ago
0 ERS 9
1 00635U 63030B 25281.42451812 -.00000018 00000-0 -10374-1 0 9998
2 00635 88.4228 228.9160 0044348 284.1662 75.4263 8.57948362948851TLE epoch observation values (Epoch: 2025-10-08T10:11:18.365Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #30 in the year 1963 (1963-07-19 UTC)
ERS 9 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. |
|---|---|---|---|---|---|---|---|
| 36 mins | 2025-12-29 01:46:15.021Z | 4.378° NNE | 2025-12-29 02:04:15.021Z | 78.234° E | 38.521° | 2025-12-29 02:22:15.021Z | 154.571° SSE |
| 33 mins | 2025-12-29 04:35:15.021Z | 351.865° N | 2025-12-29 04:51:15.021Z | 288.582° WNW | 36.312° | 2025-12-29 05:08:15.021Z | 221.467° SW |
| 22 mins | 2025-12-29 12:24:15.021Z | 92.392° ESE | 2025-12-29 12:34:15.021Z | 57.545° ENE | 20.153° | 2025-12-29 12:46:15.021Z | 16.283° NNE |
| 37 mins | 2025-12-29 14:59:15.021Z | 169.893° S | 2025-12-29 15:17:15.021Z | 104.172° ESE | 44.8° | 2025-12-29 15:36:15.021Z | 1.609° NNE |
| 29 mins | 2025-12-29 17:54:15.021Z | 244.259° WSW | 2025-12-29 18:08:15.021Z | 294.879° NW | 24.04° | 2025-12-29 18:23:15.021Z | 348.584° 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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