NIMBUS 2 DEB, 40646

Orbit data source: Space-Track

NIMBUS 2 DEB, 40646 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
40646, 1966-040BK
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Icon of a cake. It is the launch day of the satellite!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: 6 days ago

TLE from 6 days ago
0 NIMBUS 2 DEB
1 40646U 66040BK  26130.14137827  .00001389  00000-0  22767-2 0  9998
2 40646 100.3723  22.3523 0044740 218.9206 140.8702 13.49109280538849
Epoch: 2026-05-10T03:23Z
TLE epoch observation values (Epoch: 2026-05-10T03:23:35.082Z)
Latitude
0.00002°
Longitude
103.5074°
Altitude
1,104.23 km
Speed
7.288 km/s
True Right ascension
01h 29m 24s
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
05:35:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,106.211 km
Perigee altitude
1,039.54 km
Semi-major axis
7,451.013 km
Eccentricity
0.00447
Inclination
100.3723°
RAAN
22.3523°
Arg. of periapsis
218.9206°
True anomaly
141.19234°
Mean anomaly
140.8702°
Eccentric anomaly
141.03141°
Mean motion
3.37458 °/min
Orbital period
106.68 mins
BSTAR
0.0022767
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