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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https://www.satcat.com/sats-embedded/13666?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

13666, 1982-110E

Orbit

HEO

Last TLE update

3 days ago

Origin

Telesat (US)

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

Sphere + Cone, 0.9 m

Radar Cross Section

2.046 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 3 days ago

0 ANIK C3 R/B(PAM-D)
1 13666U 82110E   25194.78366651  .00000623  00000-0  86581-3 0  9999
2 13666  23.3891  64.5108 7058959 235.8460  36.8598  2.51460583328786

Epoch: 2025-07-13T18:48Z

TLE epoch observation values (Epoch: 2025-07-13T18:48:28.786Z)

Latitude

-0.00009°

Longitude

-149.42087°

Altitude

12,609.38 km

Speed

4.953 km/s

True Right ascension

04h 18m 24s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

13.19219°

Longitude

-117.89065°

Altitude

26,410.874 km

Speed

2.62 km/s

Apparent Right ascension

06h 49m 23s

Apparent Declination

6° 51' 51"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

03:49:47

Azimuth

117.161° SE

Elevation

38.029°

Doppler factor

Orbital elements

Apogee altitude

32,596.923 km

Perigee altitude

341.338 km

Semi-major axis

22,847.267 km

Eccentricity

0.7059

Inclination

23.3891°

RAAN

64.5108°

Arg. of periapsis

235.846°

True anomaly

Unknown

Mean anomaly

36.8598°

Eccentric anomaly

Unknown

Mean motion

0.62848 °/min

Orbital period

572.81 mins

BSTAR

0.00086581

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Other satellites on launch #110 in the year 1982 (1982-11-11 UTC)

STS 5, 13650 (Decayed)

SBS 3, 13651

ANIK C3 (TELESAT-5), 13652

SBS 3 R/B(PAM-D), 13658

ANIK C3 R/B(PAM-D) Visibility forecast

Observer location: undefined°, undefined°

Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
388 mins	2025-07-16 15:11:25.225Z	117.185° SE	2025-07-16 19:43:25.225Z	130.528° SE	41.28°	2025-07-16 21:39:25.225Z	104.828° ESE

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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Check out ANIK C3 R/B(PAM-D), 13666 on other resources

View ANIK C3 R/B(PAM-D), 13666 on Heavens-Above

View ANIK C3 R/B(PAM-D), 13666 on Keep Track

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

View ANIK C3 R/B(PAM-D), 13666 on Gunter's Space Page

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