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)
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
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 NIMBUS 2 DEB
1 40646U 66040BK  25259.37623962  .00001681  00000-0  27775-2 0  9993
2 40646 100.3660 137.7307 0053122  61.6009 299.0463 13.48055120507061
Epoch: 2025-09-16T09:01Z
TLE epoch observation values (Epoch: 2025-09-16T09:01:47.103Z)
Latitude
0.00005°
Longitude
6.717°
Altitude
1,063.106 km
Speed
7.33 km/s
True Right ascension
09h 10m 55s
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
23:08:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,116.364 km
Perigee altitude
1,037.16 km
Semi-major axis
7,454.899 km
Eccentricity
0.00531
Inclination
100.366°
RAAN
137.7307°
Arg. of periapsis
61.6009°
True anomaly
298.51242°
Mean anomaly
299.0463°
Eccentric anomaly
298.77953°
Mean motion
3.37195 °/min
Orbital period
106.76 mins
BSTAR
0.0027775
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