NIMBUS 2 DEB, 38182

Orbit data source: Space-Track

NIMBUS 2 DEB, 38182 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
38182, 1966-040BA
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: 2 days ago

TLE from 2 days ago
0 NIMBUS 2 DEB
1 38182U 66040BA  26257.93346554  .00003286  00000-0  42866-2 0  9996
2 38182 100.4900 320.4747 0080898 142.0020  38.0405 13.61242633619453
Epoch: 2026-09-14T22:24Z
TLE epoch observation values (Epoch: 2026-09-14T22:24:11.422Z)
Latitude
-0.72458°
Longitude
170.38698°
Altitude
987.019 km
Speed
7.381 km/s
True Right ascension
09h 21m 21s
True Declination
0° 43' 13"
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
05:08:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,088.426 km
Perigee altitude
968.59 km
Semi-major axis
7,406.645 km
Eccentricity
0.00809
Inclination
100.49°
RAAN
320.4747°
Arg. of periapsis
142.002°
True anomaly
38.61632°
Mean anomaly
38.0405°
Eccentric anomaly
38.32795°
Mean motion
3.40495 °/min
Orbital period
105.73 mins
BSTAR
0.0042866
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