NIMBUS 2 DEB, 31579

Orbit data source: Space-Track

NIMBUS 2 DEB, 31579 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
31579, 1966-040AR
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1966-05-15 (60 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: 11 hours ago

TLE from 11 hours ago
0 NIMBUS 2 DEB
1 31579U 66040AR  25334.87076521  .00002323  00000-0  37082-2 0  9996
2 31579 100.5080 300.0087 0045956 270.1260 119.5072 13.49938787909592
Epoch: 2025-11-30T20:53Z
TLE epoch observation values (Epoch: 2025-11-30T20:53:54.114Z)
Latitude
29.58411°
Longitude
-89.45862°
Altitude
1,093.019 km
Speed
7.3 km/s
True Right ascension
19h 35m 58s
True Declination
29° 26' 36"
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
05:08:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,104.056 km
Perigee altitude
1,035.6 km
Semi-major axis
7,447.965 km
Eccentricity
0.0046
Inclination
100.508°
RAAN
300.0087°
Arg. of periapsis
270.126°
True anomaly
119.96421°
Mean anomaly
119.5072°
Eccentric anomaly
119.73584°
Mean motion
3.37666 °/min
Orbital period
106.61 mins
BSTAR
0.0037082
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