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 (60 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
FRUST, 1.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 THOR BURNER 2 R/B
1 02422U 66082B   26257.40822142  .00000191  00000-0  61618-4 0  9994
2 02422  98.2566  49.8537 0108777 295.3571  63.6389 14.46822975128178
Epoch: 2026-09-14T09:47Z
TLE epoch observation values (Epoch: 2026-09-14T09:47:50.330Z)
Latitude
-0.00007°
Longitude
-90.49495°
Altitude
705.322 km
Speed
7.521 km/s
True Right ascension
03h 19m 24s
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
13:02:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
810.499 km
Perigee altitude
655.791 km
Semi-major axis
7,111.282 km
Eccentricity
0.01088
Inclination
98.2566°
RAAN
49.8537°
Arg. of periapsis
295.3571°
True anomaly
64.76248°
Mean anomaly
63.6389°
Eccentric anomaly
64.20002°
Mean motion
3.61927 °/min
Orbital period
99.47 mins
BSTAR
0.000061618
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Other satellites on launch #82 in the year 1966 (1966-09-16 UTC)

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