NIMBUS 2 DEB, 28201

Orbit data source: Space-Track

NIMBUS 2 DEB, 28201 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
28201, 1966-040P
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: 17 hours ago

TLE from 17 hours ago
0 NIMBUS 2 DEB
1 28201U 66040P   25334.69469255  .00002879  00000-0  38100-2 0  9992
2 28201 100.2642 243.5273 0053270  99.6845 290.9259 13.61217334624205
Epoch: 2025-11-30T16:40Z
TLE epoch observation values (Epoch: 2025-11-30T16:40:21.436Z)
Latitude
29.55963°
Longitude
-82.23107°
Altitude
1,020.922 km
Speed
7.351 km/s
True Right ascension
15h 50m 39s
True Declination
29° 25' 03"
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
06:58:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,068.043 km
Perigee altitude
989.132 km
Semi-major axis
7,406.725 km
Eccentricity
0.00533
Inclination
100.2642°
RAAN
243.5273°
Arg. of periapsis
99.6845°
True anomaly
290.35438°
Mean anomaly
290.9259°
Eccentric anomaly
290.64028°
Mean motion
3.4049 °/min
Orbital period
105.73 mins
BSTAR
0.00381
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