NIMBUS 2 DEB, 26669

Orbit data source: Space-Track

NIMBUS 2 DEB, 26669 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
26669, 1966-040J
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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 NIMBUS 2 DEB
1 26669U 66040J   26171.40152014  .00003793  00000-0  31507-2 0  9999
2 26669 100.1296 220.1768 0039038 164.3759 214.1302 13.89015581290302
Epoch: 2026-06-20T09:38Z
TLE epoch observation values (Epoch: 2026-06-20T09:38:11.340Z)
Latitude
17.95501°
Longitude
163.71117°
Altitude
958.01 km
Speed
7.362 km/s
True Right ascension
14h 27m 30s
True Declination
17° 51' 26"
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
03:48:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
957.882 km
Perigee altitude
900.828 km
Semi-major axis
7,307.492 km
Eccentricity
0.0039
Inclination
100.1296°
RAAN
220.1768°
Arg. of periapsis
164.3759°
True anomaly
213.88022°
Mean anomaly
214.1302°
Eccentric anomaly
214.00511°
Mean motion
3.47449 °/min
Orbital period
103.61 mins
BSTAR
0.0031507
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