THOR BURNER 2 R/B, 2422

Orbit data source: Space-Track

THOR BURNER 2 R/B, 2422 is space debris in SSO originally from a launch on Fri, 16 Sep 1966 UTC launched 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
2422, 1966-082B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 37, Unknown motor
Mass
136 kg wet, 136 kg dry
Launch date (UTC)
1966-09-16 (59 years ago)
Launch vehicle
Unknown
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: 7 hours ago

TLE from 7 hours ago
0 THOR BURNER 2 R/B
1  2422U 66082B   25296.16284933  .00001053  00000-0  28371-3 0  9995
2  2422  98.2148  92.6460 0109974 209.7259 149.7656 14.46480853 81005
Epoch: 2025-10-23T03:54Z
TLE epoch observation values (Epoch: 2025-10-23T03:54:30.182Z)
Latitude
-0.00002°
Longitude
2.19419°
Altitude
807.967 km
Speed
7.414 km/s
True Right ascension
06h 10m 35s
True Declination
0° 00' 00"
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
05:38:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
812.483 km
Perigee altitude
656.047 km
Semi-major axis
7,112.402 km
Eccentricity
0.011
Inclination
98.2148°
RAAN
92.646°
Arg. of periapsis
209.7259°
True anomaly
150.3927°
Mean anomaly
149.7656°
Eccentric anomaly
150.07989°
Mean motion
3.61842 °/min
Orbital period
99.49 mins
BSTAR
0.00028371
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Other satellites on launch #82 in the year 1966 (1966-09-16 UTC)

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