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
FRUST, 1.1 m
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 BURNER 2 R/B
1  3522U 68092B   26307.38821781  .00000094  00000-0  52767-4 0  9997
2  3522  98.8355 101.3525 0029734 119.6329 240.7820 14.31080815 20191
Epoch: 2026-11-03T09:19Z
TLE epoch observation values (Epoch: 2026-11-03T09:19:02.018Z)
Latitude
-0.0001°
Longitude
-81.05749°
Altitude
801.498 km
Speed
7.447 km/s
True Right ascension
06h 45m 24s
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
20:14:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
806.57 km
Perigee altitude
763.971 km
Semi-major axis
7,163.407 km
Eccentricity
0.00297
Inclination
98.8355°
RAAN
101.3525°
Arg. of periapsis
119.6329°
True anomaly
240.48516°
Mean anomaly
240.782°
Eccentric anomaly
240.63353°
Mean motion
3.57984 °/min
Orbital period
100.56 mins
BSTAR
0.000052767
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Other satellites on launch #92 in the year 1968 (1968-10-23 UTC)

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