NIMBUS 2 DEB, 28619

Orbit data source: Space-Track

NIMBUS 2 DEB, 28619 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
28619, 1966-040AJ
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: 1 day ago

TLE from 1 day ago
0 NIMBUS 2 DEB
1 28619U 66040AJ  25294.25198471  .00010947  00000-0  95071-2 0  9996
2 28619 100.3200  86.6979 0036777 152.3520 331.6949 13.85932301551671
Epoch: 2025-10-21T06:02Z
TLE epoch observation values (Epoch: 2025-10-21T06:02:51.478Z)
Latitude
54.89591°
Longitude
160.97413°
Altitude
928.212 km
Speed
7.405 km/s
True Right ascension
18h 46m 31s
True Declination
54° 44' 16"
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
08:06:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
967.122 km
Perigee altitude
913.293 km
Semi-major axis
7,318.345 km
Eccentricity
0.00368
Inclination
100.32°
RAAN
86.6979°
Arg. of periapsis
152.352°
True anomaly
331.49426°
Mean anomaly
331.6949°
Eccentric anomaly
331.59466°
Mean motion
3.46676 °/min
Orbital period
103.84 mins
BSTAR
0.0095071
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