NIMBUS 2 DEB, 26962

Orbit data source: Space-Track

NIMBUS 2 DEB, 26962 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
26962, 1966-040M
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: 19 hours ago

TLE from 19 hours ago
0 NIMBUS 2 DEB
1 26962U 66040M   25286.76401690  .00000320  00000-0  53798-3 0  9997
2 26962 100.2954 182.9026 0055913  29.2292   4.3738 13.53922346194271
Epoch: 2025-10-13T18:20Z
TLE epoch observation values (Epoch: 2025-10-13T18:20:11.060Z)
Latitude
33.10343°
Longitude
-121.47174°
Altitude
1,020.572 km
Speed
7.365 km/s
True Right ascension
11h 44m 32s
True Declination
32° 57' 07"
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
08:11:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,096.752 km
Perigee altitude
1,013.628 km
Semi-major axis
7,433.327 km
Eccentricity
0.00559
Inclination
100.2954°
RAAN
182.9026°
Arg. of periapsis
29.2292°
True anomaly
4.42301°
Mean anomaly
4.3738°
Eccentric anomaly
4.39837°
Mean motion
3.38663 °/min
Orbital period
106.3 mins
BSTAR
0.00053798
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