THOR BURNER 2 R/B, 3522

Orbit data source: Space-Track

THOR BURNER 2 R/B, 3522 is space debris in SSO originally from a launch on Wed, 23 Oct 1968 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
3522, 1968-092B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 37, Unknown motor
Mass
154 kg wet, 154 kg dry
Launch date (UTC)
1968-10-23 (58 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: 1 week ago

TLE from 1 week ago
0 THOR BURNER 2 R/B
1 03522U 68092B   26155.03665505  .00000208  00000-0  96021-4 0  9998
2 03522  98.8158 306.6505 0028430 203.8940 156.0925 14.31031015998396
Epoch: 2026-06-04T00:52Z
TLE epoch observation values (Epoch: 2026-06-04T00:52:46.996Z)
Latitude
0.00005°
Longitude
40.96799°
Altitude
809.852 km
Speed
7.439 km/s
True Right ascension
20h 26m 36s
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
03:09:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
805.802 km
Perigee altitude
765.07 km
Semi-major axis
7,163.573 km
Eccentricity
0.00284
Inclination
98.8158°
RAAN
306.6505°
Arg. of periapsis
203.894°
True anomaly
156.2241°
Mean anomaly
156.0925°
Eccentric anomaly
156.15834°
Mean motion
3.57972 °/min
Orbital period
100.57 mins
BSTAR
0.000096021
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Other satellites on launch #92 in the year 1968 (1968-10-23 UTC)

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