NIMBUS 2 DEB, 37888

Orbit data source: Space-Track

NIMBUS 2 DEB, 37888 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
37888, 1966-040AT
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: 10 hours ago

TLE from 10 hours ago
0 NIMBUS 2 DEB
1 37888U 66040AT  25287.00070434  .00002273  00000-0  36716-2 0  9991
2 37888 100.6155 302.5765 0049378  99.8674 291.0342 13.49166922802909
Epoch: 2025-10-14T00:01Z
TLE epoch observation values (Epoch: 2025-10-14T00:01:00.854Z)
Latitude
29.84991°
Longitude
-86.61504°
Altitude
1,065.86 km
Speed
7.328 km/s
True Right ascension
19h 45m 44s
True Declination
29° 42' 28"
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
04:40:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,109.467 km
Perigee altitude
1,035.886 km
Semi-major axis
7,450.814 km
Eccentricity
0.00494
Inclination
100.6155°
RAAN
302.5765°
Arg. of periapsis
99.8674°
True anomaly
290.50491°
Mean anomaly
291.0342°
Eccentric anomaly
290.76967°
Mean motion
3.37472 °/min
Orbital period
106.68 mins
BSTAR
0.0036716
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