NIMBUS 2 DEB, 28610

Orbit data source: Space-Track

NIMBUS 2 DEB, 28610 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
28610, 1966-040Z
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: 2 weeks ago

TLE from 2 weeks ago
0 NIMBUS 2 DEB
1 28610U 66040Z   25280.95143567  .00002238  00000-0  29751-2 0  9991
2 28610 100.5044 350.8248 0074124  39.8676 143.4585 13.60733771592453
Epoch: 2025-10-07T22:50Z
TLE epoch observation values (Epoch: 2025-10-07T22:50:04.041Z)
Latitude
-3.89788°
Longitude
170.75483°
Altitude
1,080.676 km
Speed
7.29 km/s
True Right ascension
11h 20m 25s
True Declination
-3° 52' 32"
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
06:33:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,085.271 km
Perigee altitude
975.442 km
Semi-major axis
7,408.494 km
Eccentricity
0.00741
Inclination
100.5044°
RAAN
350.8248°
Arg. of periapsis
39.8676°
True anomaly
143.96049°
Mean anomaly
143.4585°
Eccentric anomaly
143.70987°
Mean motion
3.40368 °/min
Orbital period
105.77 mins
BSTAR
0.0029751
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