TIROS 4, 226
Orbit data source: Space-Track
TIROS 4, 226 is a payload satellite owned by GSFC (US) in LEO that was launched on Thu, 08 Feb 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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226 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 TIROS 4
1 226U 62002A 26125.49970954 .00000029 00000-0 53962-4 0 9993
2 226 48.2949 204.0057 0075519 76.3550 284.5745 14.47172025362266TLE epoch observation values (Epoch: 2026-05-05T11:59:34.904Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)
TIROS 4 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-06 08:03:50.911Z | 220.639° SW | 2026-05-06 08:07:50.911Z | 127.096° SE | 41.005° | 2026-05-06 08:11:50.911Z | 65.44° ENE |
| 7 mins | 2026-05-06 09:48:50.911Z | 279.931° WNW | 2026-05-06 09:51:50.911Z | 339.342° N | 33.623° | 2026-05-06 09:55:50.911Z | 50.144° ENE |
| 7 mins | 2026-05-06 11:33:50.911Z | 310.004° NW | 2026-05-06 11:36:50.911Z | 1.076° NNE | 26.94° | 2026-05-06 11:40:50.911Z | 62.894° ENE |
| 7 mins | 2026-05-06 13:18:50.911Z | 313.275° NW | 2026-05-06 13:21:50.911Z | 25.521° NE | 39.211° | 2026-05-06 13:25:50.911Z | 99.202° ESE |
| 7 mins | 2026-05-06 15:02:50.911Z | 279.483° WNW | 2026-05-06 15:05:50.911Z | 222.239° SW | 32.191° | 2026-05-06 15:09:50.911Z | 156.305° 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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