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 (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: 1 month ago

TLE from 1 month ago
0 NIMBUS 2 DEB
1 28619U 66040AJ  25295.38837352  .00009734  00000-0  84580-2 0  9994
2 28619 100.3209  87.9583 0035860 149.9321 241.0961 13.85959515551830
Epoch: 2025-10-22T09:19Z
TLE epoch observation values (Epoch: 2025-10-22T09:19:15.472Z)
Latitude
30.17345°
Longitude
-88.96475°
Altitude
959.277 km
Speed
7.368 km/s
True Right ascension
05h 27m 38s
True Declination
30° 01' 42"
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
08:39:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
966.355 km
Perigee altitude
913.869 km
Semi-major axis
7,318.249 km
Eccentricity
0.00359
Inclination
100.3209°
RAAN
87.9583°
Arg. of periapsis
149.9321°
True anomaly
240.73714°
Mean anomaly
241.0961°
Eccentric anomaly
240.91654°
Mean motion
3.46683 °/min
Orbital period
103.84 mins
BSTAR
0.008458
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