NIMBUS 2 DEB, 26816

Orbit data source: Space-Track

NIMBUS 2 DEB, 26816 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
26816, 1966-040L
Orbit
SSO
Country
Flag of USUS
Related business
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 shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago
0 NIMBUS 2 DEB
1 26816U 66040L   25286.75354796  .00003154  00000-0  44437-2 0  9995
2 26816 100.3462 215.6006 0065465  10.2479  19.2877 13.56963432210470
Epoch: 2025-10-13T18:05Z
TLE epoch observation values (Epoch: 2025-10-13T18:05:06.543Z)
Latitude
29.30225°
Longitude
-84.07866°
Altitude
1,004.414 km
Speed
7.375 km/s
True Right ascension
13h 59m 00s
True Declination
29° 09' 38"
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
08:13:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,092.664 km
Perigee altitude
995.485 km
Semi-major axis
7,422.212 km
Eccentricity
0.00655
Inclination
100.3462°
RAAN
215.6006°
Arg. of periapsis
10.2479°
True anomaly
19.53742°
Mean anomaly
19.2877°
Eccentric anomaly
19.41237°
Mean motion
3.39424 °/min
Orbital period
106.06 mins
BSTAR
0.0044437
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