SL-12 R/B(AUX MOTOR), 20082

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 20082 is space debris in HEO originally from a launch on Wed, 31 May 1989 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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/20082?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

20082, 1989-039H

Orbit

HEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

NPO Energiya

Mission

Spacecraft

Bus & Motor

SOZ, Unknown motor

Mass

Wet unknown, ~60 kg dry

Launch date (UTC)

1989-05-31 (37 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 0.6 m

Radar Cross Section

0.660 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago

0 SL-12 R/B(AUX MOTOR)
1 20082U 89039H   25344.42536633 -.00000006  00000-0 -12060-3 0  9991
2 20082  65.0492  78.6105 5538236 102.4856 321.8980  4.42414968575409

Epoch: 2025-12-10T10:12Z

TLE epoch observation values (Epoch: 2025-12-10T10:12:31.650Z)

Latitude

0.00001°

Longitude

-153.91393°

Altitude

5,958.732 km

Speed

6.261 km/s

True Right ascension

05h 14m 27s

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

15:39:22

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

17,974.865 km

Perigee altitude

614.764 km

Semi-major axis

15,672.952 km

Eccentricity

0.55382

Inclination

65.0492°

RAAN

78.6105°

Arg. of periapsis

102.4856°

True anomaly

257.567°

Mean anomaly

321.898°

Eccentric anomaly

292.60371°

Mean motion

1.10616 °/min

Orbital period

325.45 mins

BSTAR

-0.0001206

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Other satellites on launch #39 in the year 1989 (1989-05-31 UTC)

SL-12 DEB, 29321

SL-12 DEB, 29332 (Decayed)

SL-12 DEB, 29515 (Decayed)

SL-12 DEB, 29427 (Decayed)

SL-12 DEB, 29342 (Decayed)

SL-12 DEB, 29418

SL-12 DEB, 29514 (Decayed)

SL-12 DEB, 29430

SL-12 DEB, 29469 (Decayed)

SL-12 DEB, 29449

SL-12 DEB, 29339

SL-12 DEB, 29309 (Decayed)

SL-12 DEB, 29453

SL-12 DEB, 29313 (Decayed)

SL-12 DEB, 29312

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SL-12 R/B(AUX MOTOR) 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.
34 mins	2025-12-11 07:46:05.732Z	202.677° SW	2025-12-11 08:14:05.732Z	163.136° S	44.701°	2025-12-11 08:20:05.732Z	34.389° NE

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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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Check out SL-12 R/B(AUX MOTOR), 20082 on other resources

View SL-12 R/B(AUX MOTOR), 20082 on Heavens-Above

View SL-12 R/B(AUX MOTOR), 20082 on Keep Track

View SL-12 R/B(AUX MOTOR), 20082 on Celestrak

View SL-12 R/B(AUX MOTOR), 20082 on Gunter's Space Page

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

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