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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: 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 14.47172025362266
Epoch: 2026-05-05T11:59Z
TLE epoch observation values (Epoch: 2026-05-05T11:59:34.904Z)
Latitude
-0.00001°
Longitude
160.73659°
Altitude
722.118 km
Speed
7.503 km/s
True Right ascension
13h 36m 01s
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
05:49:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
789.644 km
Perigee altitude
682.195 km
Semi-major axis
7,114.057 km
Eccentricity
0.00755
Inclination
48.2949°
RAAN
204.0057°
Arg. of periapsis
76.355°
True anomaly
283.735°
Mean anomaly
284.5745°
Eccentric anomaly
284.15495°
Mean motion
3.61716 °/min
Orbital period
99.53 mins
BSTAR
0.000053962
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Other satellites on launch #2 in the year 1962 (1962-02-08 UTC)

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