NIMBUS 2 DEB, 25526

Orbit data source: Space-Track

NIMBUS 2 DEB, 25526 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
25526, 1966-040D
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: 5 hours ago

TLE from 5 hours ago
0 NIMBUS 2 DEB
1 25526U 66040D   26128.28394304  .00002972  00000-0  28828-2 0  9998
2 25526 100.5827 238.5039 0042252 222.9225 194.4741 13.80211854660100
Epoch: 2026-05-08T06:48Z
TLE epoch observation values (Epoch: 2026-05-08T06:48:52.678Z)
Latitude
55.88852°
Longitude
-105.75999°
Altitude
1,002.374 km
Speed
7.341 km/s
True Right ascension
14h 50m 18s
True Declination
55° 44' 02"
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
20:18:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
991.451 km
Perigee altitude
929.438 km
Semi-major axis
7,338.582 km
Eccentricity
0.00423
Inclination
100.5827°
RAAN
238.5039°
Arg. of periapsis
222.9225°
True anomaly
194.3537°
Mean anomaly
194.4741°
Eccentric anomaly
194.41384°
Mean motion
3.45243 °/min
Orbital period
104.27 mins
BSTAR
0.0028828
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