TELSTAR 1, 340
Orbit data source: Space-Track
TELSTAR 1, 340 is a payload satellite owned by AT&T (US) in LEO that was launched on Tue, 10 Jul 1962 UTC via a THOR DELTA 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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340 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 TELSTAR 1
1 00340U 62029A 25258.91878677 -.00000103 00000-0 -59397-3 0 9993
2 00340 44.8028 110.3666 2424996 317.0246 36.6079 9.12886759107405
TLE epoch observation values (Epoch: 2025-09-15T22:03:03.176Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #29 in the year 1962 (1962-07-10 UTC)
TELSTAR 1 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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49 mins | 2025-09-16 19:13:44.726Z | 261.312° W | 2025-09-16 19:29:44.726Z | 349.649° N | 44.568° | 2025-09-16 20:02:44.726Z | 80.632° E |
59 mins | 2025-09-16 22:03:44.726Z | 289.466° WNW | 2025-09-16 22:26:44.726Z | 349.951° N | 44.972° | 2025-09-16 23:02:44.726Z | 117.56° SE |
58 mins | 2025-09-17 00:54:44.726Z | 296.109° NW | 2025-09-17 01:22:44.726Z | 231.773° WSW | 39.065° | 2025-09-17 01:52:44.726Z | 162.818° S |
24 mins | 2025-09-17 03:58:44.726Z | 275.436° WNW | 2025-09-17 04:10:44.726Z | 254.5° W | 13.813° | 2025-09-17 04:22:44.726Z | 231.857° WSW |
30 mins | 2025-09-17 16:08:44.726Z | 201.73° SSW | 2025-09-17 16:17:44.726Z | 129.142° SE | 39.194° | 2025-09-17 16:38:44.726Z | 63.109° ENE |
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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