NIMBUS 2 DEB, 24956

Orbit data source: Space-Track

NIMBUS 2 DEB, 24956 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
24956, 1966-040C
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: 9 hours ago

TLE from 9 hours ago
0 NIMBUS 2 DEB
1 24956U 66040C   26134.05555147  .00001469  00000-0  18660-2 0  9993
2 24956 100.4729 321.7062 0045612 117.8048   5.5674 13.64970646934738
Epoch: 2026-05-14T01:19Z
TLE epoch observation values (Epoch: 2026-05-14T01:19:59.647Z)
Latitude
55.25663°
Longitude
-94.72367°
Altitude
993.15 km
Speed
7.377 km/s
True Right ascension
10h 28m 19s
True Declination
55° 06' 02"
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
19:05:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,048.727 km
Perigee altitude
981.284 km
Semi-major axis
7,393.142 km
Eccentricity
0.00456
Inclination
100.4729°
RAAN
321.7062°
Arg. of periapsis
117.8048°
True anomaly
5.6184°
Mean anomaly
5.5674°
Eccentric anomaly
5.59287°
Mean motion
3.41428 °/min
Orbital period
105.44 mins
BSTAR
0.001866
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