NIMBUS 2 DEB, 28618

Orbit data source: Space-Track

NIMBUS 2 DEB, 28618 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
28618, 1966-040AH
Orbit
SSO
Last TLE update
6 days ago
Origin
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
Radar Cross Section
Small (<0.1 m²)

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TLE from 6 days ago
0 NIMBUS 2 DEB
1 28618U 66040AH  25193.66589469  .00004291  00000-0  33046-2 0  9998
2 28618 100.2862 338.0842 0033042 280.1842  94.3282 13.93375166602124
Epoch: 2025-07-12T15:58Z
TLE epoch observation values (Epoch: 2025-07-12T15:58:53.301Z)
Latitude
14.61964°
Longitude
164.86278°
Altitude
920.834 km
Speed
7.392 km/s
True Right ascension
22h 21m 32s
True Declination
14° 32' 16"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
31.70057°
Longitude
168.18025°
Altitude
935.571 km
Speed
7.379 km/s
Apparent Right ascension
23h 25m 37s
Apparent Declination
-1° 18' 46"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:30:34
Azimuth
25.04° NE
Elevation
-48.669°
Doppler factor
1
Orbital elements
Apogee altitude
938.197 km
Perigee altitude
890.007 km
Semi-major axis
7,292.239 km
Eccentricity
0.0033
Inclination
100.2862°
RAAN
338.0842°
Arg. of periapsis
280.1842°
True anomaly
94.70563°
Mean anomaly
94.3282°
Eccentric anomaly
94.51693°
Mean motion
3.48539 °/min
Orbital period
103.29 mins
BSTAR
0.0033046
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