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 (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 26962U 66040M   26033.20447889  .00001292  00000-0  19496-2 0  9992
2 26962 100.3019 298.8674 0050568 124.1382  29.3645 13.54347218209356
Epoch: 2026-02-02T04:54Z
TLE epoch observation values (Epoch: 2026-02-02T04:54:26.976Z)
Latitude
25.791°
Longitude
-82.13527°
Altitude
1,026.583 km
Speed
7.357 km/s
True Right ascension
08h 15m 31s
True Declination
25° 39' 41"
Sunlit
Object was in full shadow 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
16:07:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,091.215 km
Perigee altitude
1,016.053 km
Semi-major axis
7,431.771 km
Eccentricity
0.00506
Inclination
100.3019°
RAAN
298.8674°
Arg. of periapsis
124.1382°
True anomaly
29.65022°
Mean anomaly
29.3645°
Eccentric anomaly
29.5072°
Mean motion
3.3877 °/min
Orbital period
106.27 mins
BSTAR
0.0019496
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