ANIK C2 R/B(PAM-D), 14135

Orbit data source: Space-Track

ANIK C2 R/B(PAM-D), 14135 is space debris in HEO originally from a launch on Sat, 18 Jun 1983 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
14135, 1983-059D
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 48, Unknown motor
Mass
2,154 kg wet, 191 kg dry
Launch date (UTC)
1983-06-18 (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: 2 days ago

TLE from 2 days ago
0 ANIK C2 R/B(PAM-D)
1 14135U 83059D   26061.45689721  .00001369  00000-0  13891-2 0  9999
2 14135  22.9591 180.6841 6912288 318.9504   5.8074  2.71251183318587
Epoch: 2026-03-02T10:57Z
TLE epoch observation values (Epoch: 2026-03-02T10:57:55.918Z)
Latitude
0.00005°
Longitude
-144.15199°
Altitude
1,060.44 km
Speed
9.424 km/s
True Right ascension
12h 02m 19s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
13:09:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
30,359.085 km
Perigee altitude
329.055 km
Semi-major axis
21,722.207 km
Eccentricity
0.69123
Inclination
22.9591°
RAAN
180.6841°
Arg. of periapsis
318.9504°
True anomaly
40.95908°
Mean anomaly
5.8074°
Eccentric anomaly
18.13376°
Mean motion
0.67793 °/min
Orbital period
531.03 mins
BSTAR
0.0013891
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