SL-12 R/B(AUX MOTOR), 13608

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 13608 is space debris originally from a launch on Tue, 12 Oct 1982 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/13608?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

13608, 1982-100F

Orbit

Active

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)

1982-10-12 (43 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 SL-12 R/B(AUX MOTOR)
1 13608U 82100F   26095.05024496  .00025708  00000-0  87661-3 0  9994
2 13608  52.0532 333.9086 3275450 316.0819  22.1178  8.85667002979797

Epoch: 2026-04-05T01:12Z

TLE epoch observation values (Epoch: 2026-04-05T01:12:21.164Z)

Latitude

0.00001°

Longitude

122.45919°

Altitude

752.423 km

Speed

8.452 km/s

True Right ascension

22h 15m 38s

True Declination

0° 00' 00"

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

19:30:20

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

6,722.328 km

Perigee altitude

257.776 km

Semi-major axis

9,868.189 km

Eccentricity

0.32755

Inclination

52.0532°

RAAN

333.9086°

Arg. of periapsis

316.0819°

True anomaly

44.00195°

Mean anomaly

22.1178°

Eccentric anomaly

32.08689°

Mean motion

2.21405 °/min

Orbital period

162.6 mins

BSTAR

0.00087661

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Other satellites on launch #100 in the year 1982 (1982-10-12 UTC)

SL-12 PLAT, 13605 (Decayed)

COSMOS 1413 (GLONASS), 13603

SL-12 R/B(AUX MOTOR), 13609

SL-12 R/B(1), 13604 (Decayed)

SL-12 R/B(2), 13610

COSMOS 1415 (GLONASS), 13607

COSMOS 1414 (GLONASS), 13606

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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.
32 mins	2026-04-05 17:33:20.141Z	194.551° SSW	2026-04-05 17:41:20.141Z	120.997° SE	39.469°	2026-04-05 18:05:20.141Z	51.468° ENE
52 mins	2026-04-05 20:22:20.141Z	263.225° W	2026-04-05 20:35:20.141Z	344.125° N	42.568°	2026-04-05 21:14:20.141Z	68.958° E
71 mins	2026-04-05 23:15:20.141Z	297.26° NW	2026-04-05 23:40:20.141Z	21.224° NNE	43.273°	2026-04-06 00:26:20.141Z	110.482° ESE
72 mins	2026-04-06 02:10:20.141Z	307.572° NW	2026-04-06 02:45:20.141Z	233.491° WSW	43.365°	2026-04-06 03:22:20.141Z	159.263° S
50 mins	2026-04-06 05:11:20.141Z	300.004° NW	2026-04-06 05:36:20.141Z	263.627° W	22.558°	2026-04-06 06:01:20.141Z	221.603° SW

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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 SL-12 R/B(AUX MOTOR), 13608 on other resources

View SL-12 R/B(AUX MOTOR), 13608 on Heavens-Above

View SL-12 R/B(AUX MOTOR), 13608 on Keep Track

View SL-12 R/B(AUX MOTOR), 13608 on Celestrak

View SL-12 R/B(AUX MOTOR), 13608 on Gunter's Space Page

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

SL-12 R/B(AUX MOTOR), 13608

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-04-05T01:12:21.164Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #100 in the year 1982 (1982-10-12 UTC)

SL-12 R/B(AUX MOTOR) Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-12 R/B(AUX MOTOR), 13608 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago