TIROS 1, 29
Orbit data source: Space-Track
TIROS 1, 29 is a payload satellite owned by GSFC (US) in LEO that was launched on Fri, 01 Apr 1960 UTC via a THOR ABLE II 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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29 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 TIROS 1
1 29U 60002B 26317.85770286 .00000586 00000-0 10715-3 0 9997
2 29 48.3793 33.2530 0022345 195.2700 164.7542 14.78937134564284TLE epoch observation values (Epoch: 2026-11-13T20:35:05.527Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #2 in the year 1960 (1960-04-01 UTC)
TIROS 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-14 08:07:29.744Z | 217.616° SW | 2026-11-14 08:10:29.744Z | 159.059° S | 57.759° | 2026-11-14 08:14:29.744Z | 66.997° ENE |
| 7 mins | 2026-11-14 09:49:29.744Z | 276.662° WNW | 2026-11-14 09:52:29.744Z | 330.719° NNW | 40.52° | 2026-11-14 09:56:29.744Z | 48.445° ENE |
| 7 mins | 2026-11-14 11:32:29.744Z | 309.83° NW | 2026-11-14 11:35:29.744Z | 1.379° NNE | 28.268° | 2026-11-14 11:39:29.744Z | 61.438° ENE |
| 7 mins | 2026-11-14 13:15:29.744Z | 317.877° NNW | 2026-11-14 13:18:29.744Z | 36.726° NE | 45.793° | 2026-11-14 13:22:29.744Z | 95.951° ESE |
| 6 mins | 2026-11-14 14:57:29.744Z | 280.103° WNW | 2026-11-14 15:00:29.744Z | 201.029° SSW | 42.999° | 2026-11-14 15:03:29.744Z | 151.527° SSE |
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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