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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Iframe URL

https://www.satcat.com/sats-embedded/14135?theme=dark&initialShowStats=false

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Identifier

14135, 1983-059D

Orbit

HEO

Country

Related business

Telesat (CA)

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: 19 hours ago

TLE from 19 hours ago

0 ANIK C2 R/B(PAM-D)
1 14135U 83059D   26066.24877479  .00001898  00000-0  15752-2 0  9995
2 14135  22.9572 178.4293 6910578 322.8902   5.2325  2.71268295318718

Epoch: 2026-03-07T05:58Z

TLE epoch observation values (Epoch: 2026-03-07T05:58:14.141Z)

Latitude

-0.00002°

Longitude

-76.1805°

Altitude

926.376 km

Speed

9.528 km/s

True Right ascension

11h 53m 24s

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

04:35:20

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

30,353.822 km

Perigee altitude

332.487 km

Semi-major axis

21,721.291 km

Eccentricity

0.69106

Inclination

22.9572°

RAAN

178.4293°

Arg. of periapsis

322.8902°

True anomaly

37.33668°

Mean anomaly

5.2325°

Eccentric anomaly

16.43478°

Mean motion

0.67798 °/min

Orbital period

530.99 mins

BSTAR

0.0015752

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Other satellites on launch #59 in the year 1983 (1983-06-18 UTC)

PALAPA B1 R/B(PAM-D), 14136

NAHUEL I2 (ANIK C2), 14133

SPAS 01, 14142 (Decayed)

STS 7, 14132 (Decayed)

PALAPA B1, 14134

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ANIK C2 R/B(PAM-D) Visibility forecast

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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.
93 mins	2026-03-08 08:37:52.569Z	155.504° SSE	2026-03-08 08:47:52.569Z	116.797° SE	19.217°	2026-03-08 10:10:52.569Z	81.144° E
246 mins	2026-03-08 11:05:52.569Z	82.936° E	2026-03-08 13:51:52.569Z	98.585° ESE	14.137°	2026-03-08 15:11:52.569Z	106.596° ESE
295 mins	2026-03-08 18:11:52.569Z	275.37° WNW	2026-03-08 19:38:52.569Z	263.373° W	25.557°	2026-03-08 23:06:52.569Z	262.229° W

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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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out ANIK C2 R/B(PAM-D), 14135 on other resources

View ANIK C2 R/B(PAM-D), 14135 on Heavens-Above

View ANIK C2 R/B(PAM-D), 14135 on Keep Track

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

View ANIK C2 R/B(PAM-D), 14135 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

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

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 19 hours ago

TLE from 19 hours ago

TLE epoch observation values (Epoch: 2026-03-07T05:58:14.141Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #59 in the year 1983 (1983-06-18 UTC)

ANIK C2 R/B(PAM-D) Visibility forecast

Co-orbital & Co-planar RSOs

Check out ANIK C2 R/B(PAM-D), 14135 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 19 hours ago