NIMBUS 2 DEB, 37890

Orbit data source: Space-Track

NIMBUS 2 DEB, 37890 is space debris in SSO originally from a launch on Sun, 15 May 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
37890, 1966-040AV
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1966-05-15 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 NIMBUS 2 DEB
1 37890U 66040AV  25295.85167677  .00003207  00000-0  51798-2 0  9997
2 37890 100.5119 243.3893 0053196  29.9658 330.4500 13.48667152689495
Epoch: 2025-10-22T20:26Z
TLE epoch observation values (Epoch: 2025-10-22T20:26:24.872Z)
Latitude
-0.00002°
Longitude
-94.73368°
Altitude
1,045.466 km
Speed
7.346 km/s
True Right ascension
16h 13m 33s
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
22:43:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,114.158 km
Perigee altitude
1,034.868 km
Semi-major axis
7,452.65 km
Eccentricity
0.00532
Inclination
100.5119°
RAAN
243.3893°
Arg. of periapsis
29.9658°
True anomaly
330.14762°
Mean anomaly
330.45°
Eccentric anomaly
330.29898°
Mean motion
3.37347 °/min
Orbital period
106.71 mins
BSTAR
0.0051798
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