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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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Identifier
226, 1962-002A
Orbit
LEO
Last TLE update
7 hours ago
Origin
Manufacturer
RCA/East Windsor
Mission
Non-operational Civil Weather
Bus & Motor
TIROS, Unknown motor
Mass
129 kg wet, 129 kg dry
Launch date (UTC)
1962-02-08 (63 years ago)
Launch vehicle
THOR DELTA
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.07 m
Radar Cross Section
0.853 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 7 hours ago
0 TIROS 4
1   226U 62002A   25129.08371662  .00000259  00000-0  11471-3 0  9995
2   226  48.2972  39.7247 0076298  26.6645 333.8148 14.46933932330805
Epoch: 2025-05-09T02:00Z
Definitive object data (Epoch: 2025-05-09T02:00:33.115Z)
Latitude
-0.00001°
Longitude
142.44176°
Altitude
687.412 km
Speed
7.54 km/s
True Right ascension
02h 38m 53s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude
22.35625°
Longitude
-60.31522°
Altitude
763.924 km
Speed
7.461 km/s
Apparent Right ascension
10h 10m 33s
Apparent Declination
-12° 08' 44"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
17:28:34
Azimuth
272.987° WNW
Elevation
-22.666°
Doppler factor
1
Orbital elements
Apogee altitude
790.984 km
Perigee altitude
682.415 km
Semi-major axis
7,114.836 km
Eccentricity
0.0076298
Inclination
48.2972°
RAAN
39.7247°
Arg. of periapsis
26.6645°
True anomaly
333.42566°
Mean anomaly
333.8148°
Eccentric anomaly
333.62057°
Mean motion
3.61656 °/min
BSTAR
0.00011471
Orbital period
99.54 mins
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

TIROS 4 Visibility forecast

Observer location: undefined°, undefined°

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 mins2025-05-09 20:24:16.024Z204.053° SW2025-05-09 20:28:16.024Z132.802° SE32.448°2025-05-09 20:32:16.024Z72.427° E
7 mins2025-05-09 22:09:16.024Z267.719° W2025-05-09 22:12:16.024Z341.718° N38.833°2025-05-09 22:16:16.024Z52.178° ENE
7 mins2025-05-09 23:54:16.024Z306.965° NW2025-05-09 23:57:16.024Z1.401° NNE27.443°2025-05-10 00:01:16.024Z58.506° ENE
7 mins2025-05-10 01:39:16.024Z317.291° NNW2025-05-10 01:42:16.024Z21.885° NNE34.752°2025-05-10 01:46:16.024Z87.256° E
8 mins2025-05-10 03:23:16.024Z290.58° WNW2025-05-10 03:26:16.024Z234.307° WSW40.876°2025-05-10 03:31:16.024Z138.261° SSE
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