SL-12 R/B(AUX MOTOR), 36115

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 36115 is space debris in HEO originally from a launch on Mon, 14 Dec 2009 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/36115?theme=dark&initialShowStats=false

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Identifier

36115, 2009-070E

Orbit

HEO

Country

CIS

Related business

Russian Space Forces (RU)

Manufacturer

RKKE

Mission

Spacecraft

Bus & Motor

SOZ, Unknown motor

Mass

56 kg wet, 56 kg dry

Launch date (UTC)

2009-12-14 (16 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: 2 days ago

TLE from 2 days ago

0 SL-12 R/B(AUX MOTOR)
1 36115U 09070E   25347.37017017 -.00000021  00000-0  37447-3 0  9991
2 36115  65.2967 312.6007 5629637 277.0702  25.3673  4.26795224248051

Epoch: 2025-12-13T08:53Z

TLE epoch observation values (Epoch: 2025-12-13T08:53:02.702Z)

Latitude

0.00006°

Longitude

97.0251°

Altitude

3,882.384 km

Speed

7.272 km/s

True Right ascension

20h 50m 20s

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

13:26:12

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

18,712.211 km

Perigee altitude

637.632 km

Semi-major axis

16,053.058 km

Eccentricity

0.56296

Inclination

65.2967°

RAAN

312.6007°

Arg. of periapsis

277.0702°

True anomaly

82.96892°

Mean anomaly

25.3673°

Eccentric anomaly

50.11965°

Mean motion

1.0671 °/min

Orbital period

337.36 mins

BSTAR

0.00037447

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Other satellites on launch #70 in the year 2009 (2009-12-14 UTC)

SL-12 R/B(2), 36118

SL-12 R/B(AUX MOTOR), 36116

COSMOS 2458 (GLONASS), 36113

COSMOS 2457 (GLONASS), 36112

SL-12 DEB, 45035 (Decayed)

SL-12 DEB, 45036 (Decayed)

SL-12 DEB, 36127 (Decayed)

COSMOS 2456 (GLONASS), 36111

SL-12 DEB, 45244 (Decayed)

SL-12 PLAT, 36114 (Decayed)

SL-12 DEB, 45243 (Decayed)

SL-12 R/B(1), 36117 (Decayed)

SL-12 DEB, 36128 (Decayed)

SL-12 DEB, 36126 (Decayed)

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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.
225 mins	2025-12-15 22:44:37.589Z	194.094° SSW	2025-12-15 23:17:37.589Z	106.66° ESE	44.863°	2025-12-16 02:29:37.589Z	54.134° ENE
246 mins	2025-12-16 04:59:37.589Z	299.941° NW	2025-12-16 08:14:37.589Z	72.242° E	44.889°	2025-12-16 09:05:37.589Z	156.919° SSE
116 mins	2025-12-16 12:05:37.589Z	336.382° NNW	2025-12-16 13:09:37.589Z	318.67° NNW	16.83°	2025-12-16 14:01:37.589Z	293.727° NW

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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), 36115 on other resources

View SL-12 R/B(AUX MOTOR), 36115 on Heavens-Above

View SL-12 R/B(AUX MOTOR), 36115 on Keep Track

View SL-12 R/B(AUX MOTOR), 36115 on Celestrak

View SL-12 R/B(AUX MOTOR), 36115 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), 36115

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2025-12-13T08:53:02.702Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #70 in the year 2009 (2009-12-14 UTC)

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

Co-orbital & Co-planar RSOs

Check out SL-12 R/B(AUX MOTOR), 36115 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago