ANIK C3 R/B(PAM-D), 13666

Orbit data source: Space-Track

ANIK C3 R/B(PAM-D), 13666 is space debris in HEO originally from a launch on Thu, 11 Nov 1982 UTC launched from the Air Force Eastern Test Range (AFETR). 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
13666, 1982-110E
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 48, Unknown motor
Mass
2,153 kg wet, 190 kg dry
Launch date (UTC)
1982-11-11 (43 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 ANIK C3 R/B(PAM-D)
1 13666U 82110E   26080.79767275  .00002979  00000-0  34947-2 0  9996
2 13666  23.3786 319.5003 7053390  59.6072 351.3589  2.52122766335109
Epoch: 2026-03-21T19:08Z
TLE epoch observation values (Epoch: 2026-03-21T19:08:38.925Z)
Latitude
-0.00017°
Longitude
-146.97309°
Altitude
2,035.135 km
Speed
8.79 km/s
True Right ascension
21h 18m 00s
True Declination
0° 00' 01"
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
02:55:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
32,515.958 km
Perigee altitude
342.27 km
Semi-major axis
22,807.251 km
Eccentricity
0.70534
Inclination
23.3786°
RAAN
319.5003°
Arg. of periapsis
59.6072°
True anomaly
300.04255°
Mean anomaly
351.3589°
Eccentric anomaly
333.03178°
Mean motion
0.63014 °/min
Orbital period
571.31 mins
BSTAR
0.0034947
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Other satellites on launch #110 in the year 1982 (1982-11-11 UTC)

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