THOR BURNER 2 R/B, 2940

Orbit data source: Space-Track

THOR BURNER 2 R/B, 2940 is space debris in SSO originally from a launch on Wed, 23 Aug 1967 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
2940, 1967-080B
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)
1967-08-23 (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: 22 hours ago

TLE from 22 hours ago
0 THOR BURNER 2 R/B
1 02940U 67080B   26145.39743605  .00000087  00000-0  63700-4 0  9996
2 02940  98.5390 332.9350 0036089 273.0769  86.6277 14.17258915 31762
Epoch: 2026-05-25T09:32Z
TLE epoch observation values (Epoch: 2026-05-25T09:32:18.474Z)
Latitude
-0.00006°
Longitude
-53.12778°
Altitude
836.116 km
Speed
7.436 km/s
True Right ascension
22h 11m 44s
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
17:17:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
857.812 km
Perigee altitude
805.772 km
Semi-major axis
7,209.929 km
Eccentricity
0.00361
Inclination
98.539°
RAAN
332.935°
Arg. of periapsis
273.0769°
True anomaly
87.04064°
Mean anomaly
86.6277°
Eccentric anomaly
86.83416°
Mean motion
3.54525 °/min
Orbital period
101.54 mins
BSTAR
0.0000637
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Other satellites on launch #80 in the year 1967 (1967-08-23 UTC)

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