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
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: 21 hours ago

TLE from 21 hours ago
0 NIMBUS 2 DEB
1 28618U 66040AH  26142.45027957  .00005024  00000-0  35336-2 0  9998
2 28618 100.2561 327.2710 0036442 172.3436 217.9426 13.98335942645901
Epoch: 2026-05-22T10:48Z
TLE epoch observation values (Epoch: 2026-05-22T10:48:24.154Z)
Latitude
29.55259°
Longitude
-80.76804°
Altitude
924.122 km
Speed
7.382 km/s
True Right ascension
21h 25m 39s
True Declination
29° 24' 31"
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
16:29:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
923.342 km
Perigee altitude
870.319 km
Semi-major axis
7,274.967 km
Eccentricity
0.00364
Inclination
100.2561°
RAAN
327.271°
Arg. of periapsis
172.3436°
True anomaly
217.68675°
Mean anomaly
217.9426°
Eccentric anomaly
217.81458°
Mean motion
3.49781 °/min
Orbital period
102.92 mins
BSTAR
0.0035336
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