NIMBUS 2 DEB, 28205

Orbit data source: Space-Track

NIMBUS 2 DEB, 28205 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
28205, 1966-040T
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: 13 hours ago

TLE from 13 hours ago
0 NIMBUS 2 DEB
1 28205U 66040T   25286.87909578  .00002645  00000-0  39603-2 0  9999
2 28205 100.3081 149.0622 0043015 169.8439 214.0397 13.53832400 59334
Epoch: 2025-10-13T21:05Z
TLE epoch observation values (Epoch: 2025-10-13T21:05:53.875Z)
Latitude
23.22591°
Longitude
165.45868°
Altitude
1,087.429 km
Speed
7.297 km/s
True Right ascension
09h 38m 26s
True Declination
23° 06' 25"
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
04:42:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,087.496 km
Perigee altitude
1,023.544 km
Semi-major axis
7,433.657 km
Eccentricity
0.0043
Inclination
100.3081°
RAAN
149.0622°
Arg. of periapsis
169.8439°
True anomaly
213.76501°
Mean anomaly
214.0397°
Eccentric anomaly
213.90223°
Mean motion
3.38641 °/min
Orbital period
106.31 mins
BSTAR
0.0039603
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