THOR AGENA B R/B, 426

Orbit data source: Space-Track

THOR AGENA B R/B, 426 is space debris in LEO originally from a launch on Sat, 29 Sep 1962 UTC via a THOR AGENA B launch vehicle from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
426, 1962-049B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
GSFC
Mission
Spacecraft
Bus & Motor
TAVE, Unknown motor
Mass
900 kg wet, 91 kg dry
Launch date (UTC)
1962-09-29 (63 years ago)
Launch vehicle
THOR AGENA B
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 THOR AGENA B R/B
1 00426U 62049B   25340.83852411  .00000105  00000-0  11119-3 0  9991
2 00426  80.4707  98.0939 0017662   6.6461 107.7335 13.68737297153810
Epoch: 2025-12-06T20:07Z
TLE epoch observation values (Epoch: 2025-12-06T20:07:28.483Z)
Latitude
63.84137°
Longitude
-119.51271°
Altitude
1,019.02 km
Speed
7.346 km/s
True Right ascension
17h 12m 51s
True Declination
63° 42' 35"
Sunlit
Object was in daylight 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
08:52:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,014.409 km
Perigee altitude
988.342 km
Semi-major axis
7,379.512 km
Eccentricity
0.00177
Inclination
80.4707°
RAAN
98.0939°
Arg. of periapsis
6.6461°
True anomaly
107.92614°
Mean anomaly
107.7335°
Eccentric anomaly
107.82984°
Mean motion
3.42375 °/min
Orbital period
105.15 mins
BSTAR
0.00011119
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Other satellites on launch #49 in the year 1962 (1962-09-29 UTC)

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