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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
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational spacecraft
Bus & Motor
TIROS, Unknown motor
Mass
129 kg wet, 129 kg dry
Launch date (UTC)
1962-02-08 (64 years ago)
Launch vehicle
THOR DELTA
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 TIROS 4
1   226U 62002A   25363.45234230  .00000352  00000-0  13810-3 0  9998
2   226  48.2969  59.0876 0076803 272.7015  86.5095 14.47087432343860
Epoch: 2025-12-29T10:51Z
TLE epoch observation values (Epoch: 2025-12-29T10:51:22.374Z)
Latitude
-0.00004°
Longitude
158.09457°
Altitude
732.623 km
Speed
7.492 km/s
True Right ascension
03h 56m 21s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
00:47:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
790.837 km
Perigee altitude
681.556 km
Semi-major axis
7,114.333 km
Eccentricity
0.00768
Inclination
48.2969°
RAAN
59.0876°
Arg. of periapsis
272.7015°
True anomaly
87.38844°
Mean anomaly
86.5095°
Eccentric anomaly
86.94892°
Mean motion
3.61694 °/min
Orbital period
99.53 mins
BSTAR
0.0001381
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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