NIMBUS 2 DEB, 28609

Orbit data source: Space-Track

NIMBUS 2 DEB, 28609 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
28609, 1966-040Y
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: 1 day ago

TLE from 1 day ago
0 NIMBUS 2 DEB
1 28609U 66040Y   26078.59409903  .00000922  00000-0  15102-2 0  9997
2 28609 100.3424 350.8653 0048769 183.2689 297.4491 13.50122607623095
Epoch: 2026-03-19T14:15Z
TLE epoch observation values (Epoch: 2026-03-19T14:15:30.156Z)
Latitude
58.3141°
Longitude
156.95353°
Altitude
1,064.927 km
Speed
7.333 km/s
True Right ascension
12h 31m 52s
True Declination
58° 09' 59"
Sunlit
Object was in full shadow 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
20:46:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,105.462 km
Perigee altitude
1,032.823 km
Semi-major axis
7,447.28 km
Eccentricity
0.00488
Inclination
100.3424°
RAAN
350.8653°
Arg. of periapsis
183.2689°
True anomaly
296.95177°
Mean anomaly
297.4491°
Eccentric anomaly
297.20058°
Mean motion
3.37712 °/min
Orbital period
106.6 mins
BSTAR
0.0015102
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