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

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 36116 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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<iframe src="https://www.satcat.com/sats-embedded/36116?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/36116?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

36116, 2009-070F

Orbit

HEO

Last TLE update

2 days ago

Origin

Russian Space Forces (CIS)

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, 1.1 m

Radar Cross Section

0.660 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 2 days ago

0 SL-12 R/B(AUX MOTOR)
1 36116U 09070F   25167.45480150  .00000011  00000-0  88260-4 0  9991
2 36116  64.9424 344.6317 5666013 316.4172  10.6366  4.35520444 85104

Epoch: 2025-06-16T10:54Z

TLE epoch observation values (Epoch: 2025-06-16T10:54:54.849Z)

Latitude

-0.00017°

Longitude

-84.05928°

Altitude

1,252.798 km

Speed

8.907 km/s

True Right ascension

22h 58m 32s

True Declination

0° 00' 01"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

7.4647°

Longitude

-81.34926°

Altitude

1,596.684 km

Speed

8.65 km/s

Apparent Right ascension

22h 51m 25s

Apparent Declination

-45° 09' 18"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

23:20:27

Azimuth

185.129° SSW

Elevation

4.68°

Doppler factor

Orbital elements

Apogee altitude

18,433.576 km

Perigee altitude

485.999 km

Semi-major axis

15,837.925 km

Eccentricity

0.5666

Inclination

64.9424°

RAAN

344.6317°

Arg. of periapsis

316.4172°

True anomaly

Unknown

Mean anomaly

10.6366°

Eccentric anomaly

Unknown

Mean motion

1.08892 °/min

Orbital period

330.6 mins

BSTAR

0.00008826

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

COSMOS 2456 (GLONASS), 36111

COSMOS 2457 (GLONASS), 36112

COSMOS 2458 (GLONASS), 36113

SL-12 PLAT, 36114 (Decayed)

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

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

SL-12 R/B(2), 36118

SL-12 DEB, 36126 (Decayed)

SL-12 DEB, 36127 (Decayed)

SL-12 DEB, 36128 (Decayed)

SL-12 DEB, 45034

SL-12 DEB, 45035 (Decayed)

SL-12 DEB, 45036 (Decayed)

SL-12 DEB, 45040

SL-12 R/B(AUX MOTOR) 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.
87 mins	2025-06-18 12:33:54.833Z	183.039° SSW	2025-06-18 12:44:54.833Z	104.985° ESE	42.445°	2025-06-18 14:00:54.833Z	35.302° NE
245 mins	2025-06-18 18:22:54.833Z	302.227° NW	2025-06-18 20:03:54.833Z	57.147° ENE	41.037°	2025-06-18 22:27:54.833Z	144.961° SSE
191 mins	2025-06-19 00:24:54.833Z	330.105° NNW	2025-06-19 01:46:54.833Z	295.546° NW	32.416°	2025-06-19 03:35:54.833Z	250.106° W
50 mins	2025-06-19 10:40:54.833Z	112.69° SE	2025-06-19 10:51:54.833Z	67.764° E	23.844°	2025-06-19 11:30:54.833Z	28.694° NE

Authenticating...

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Check out SL-12 R/B(AUX MOTOR), 36116 on other resources

View SL-12 R/B(AUX MOTOR), 36116 on Heavens-Above

View SL-12 R/B(AUX MOTOR), 36116 on Keep Track

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

View SL-12 R/B(AUX MOTOR), 36116 on Gunter's Space Page

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