NIMBUS 2 DEB, 28620

Orbit data source: Space-Track

NIMBUS 2 DEB, 28620 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
28620, 1966-040AK
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: 2 days ago

TLE from 2 days ago
0 NIMBUS 2 DEB
1 28620U 66040AK  26081.48249259  .00002314  00000-0  35744-2 0  9999
2 28620 100.4388 348.8634 0038797 234.0517 305.6241 13.52124761 39494
Epoch: 2026-03-22T11:34Z
TLE epoch observation values (Epoch: 2026-03-22T11:34:47.359Z)
Latitude
0.56708°
Longitude
175.2818°
Altitude
1,050.394 km
Speed
7.335 km/s
True Right ascension
11h 15m 52s
True Declination
0° 33' 50"
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
04:48:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,090.654 km
Perigee altitude
1,032.925 km
Semi-major axis
7,439.926 km
Eccentricity
0.00388
Inclination
100.4388°
RAAN
348.8634°
Arg. of periapsis
234.0517°
True anomaly
305.2617°
Mean anomaly
305.6241°
Eccentric anomaly
305.443°
Mean motion
3.38213 °/min
Orbital period
106.44 mins
BSTAR
0.0035744
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