NIMBUS 2 DEB, 28978

Orbit data source: Space-Track

NIMBUS 2 DEB, 28978 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
28978, 1966-040AP
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: 12 hours ago

TLE from 12 hours ago
0 NIMBUS 2 DEB
1 28978U 66040AP  26043.78845183  .00002014  00000-0  31175-2 0  9995
2 28978 100.3791 333.3780 0044232 328.2257  55.5666 13.52096175913115
Epoch: 2026-02-12T18:55Z
TLE epoch observation values (Epoch: 2026-02-12T18:55:22.238Z)
Latitude
23.81458°
Longitude
-97.9126°
Altitude
1,048.784 km
Speed
7.339 km/s
True Right ascension
21h 55m 03s
True Declination
23° 41' 34"
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
09:54:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,094.8 km
Perigee altitude
1,028.982 km
Semi-major axis
7,440.028 km
Eccentricity
0.00442
Inclination
100.3791°
RAAN
333.378°
Arg. of periapsis
328.2257°
True anomaly
55.98596°
Mean anomaly
55.5666°
Eccentric anomaly
55.77615°
Mean motion
3.38206 °/min
Orbital period
106.44 mins
BSTAR
0.0031175
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