NIMBUS 2 DEB, 25614

Orbit data source: Space-Track

NIMBUS 2 DEB, 25614 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
25614, 1966-040G
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: 15 hours ago

TLE from 15 hours ago
0 NIMBUS 2 DEB
1 25614U 66040G   26060.48538900  .00002570  00000-0  33418-2 0  9990
2 25614 100.5129 243.1402 0053390 350.7561  65.8612 13.62476698455184
Epoch: 2026-03-01T11:38Z
TLE epoch observation values (Epoch: 2026-03-01T11:38:57.609Z)
Latitude
55.8137°
Longitude
-106.66299°
Altitude
1,019.882 km
Speed
7.355 km/s
True Right ascension
15h 09m 28s
True Declination
55° 39' 34"
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
06:16:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,063.553 km
Perigee altitude
984.513 km
Semi-major axis
7,402.17 km
Eccentricity
0.00534
Inclination
100.5129°
RAAN
243.1402°
Arg. of periapsis
350.7561°
True anomaly
66.42103°
Mean anomaly
65.8612°
Eccentric anomaly
66.14096°
Mean motion
3.40804 °/min
Orbital period
105.63 mins
BSTAR
0.0033418
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