SL-12 R/B(AUX MOTOR), 29680

Orbit data source: Space-Track

SL-12 R/B(AUX MOTOR), 29680 is space debris in HEO originally from a launch on Mon, 25 Dec 2006 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/29680?theme=dark&initialShowStats=false

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Identifier

29680, 2006-062G

Orbit

HEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

RKKE

Mission

Spacecraft

Bus & Motor

SOZ, Unknown motor

Mass

56 kg wet, 56 kg dry

Launch date (UTC)

2006-12-25 (19 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: 1 day ago

TLE from 1 day ago

0 SL-12 R/B(AUX MOTOR)
1 29680U 06062G   26033.37108756  .00000208  00000-0  63412-3 0  9999
2 29680  65.1459  83.6750 5709705 217.6380  83.9625  4.25914475194699

Epoch: 2026-02-02T08:54Z

TLE epoch observation values (Epoch: 2026-02-02T08:54:21.965Z)

Latitude

0.00002°

Longitude

177.52877°

Altitude

13,404.169 km

Speed

3.938 km/s

True Right ascension

05h 34m 45s

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

17:28:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

18,875.491 km

Perigee altitude

518.588 km

Semi-major axis

16,075.176 km

Eccentricity

0.57097

Inclination

65.1459°

RAAN

83.675°

Arg. of periapsis

217.638°

True anomaly

142.42634°

Mean anomaly

83.9625°

Eccentric anomaly

113.87692°

Mean motion

1.0649 °/min

Orbital period

338.06 mins

BSTAR

0.00063412

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Other satellites on launch #62 in the year 2006 (2006-12-25 UTC)

SL-12 DEB, 44984

SL-12 DEB, 44982

COSMOS 2426 (GLONASS), 29671

SL-12 R/B(1), 29674 (Decayed)

COSMOS 2424 (GLONASS), 29672

SL-12 R/B(2), 29673

SL-12 PLAT, 29675 (Decayed)

SL-12 R/B(AUX MOTOR), 29682

COSMOS 2425 (GLONASS), 29670

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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.
37 mins	2026-02-03 16:30:54.989Z	329.715° NNW	2026-02-03 16:57:54.989Z	295.242° NW	19.913°	2026-02-03 17:07:54.989Z	253.57° W
208 mins	2026-02-04 00:18:54.989Z	120.272° SE	2026-02-04 02:23:54.989Z	69.026° E	36.263°	2026-02-04 03:46:54.989Z	30.501° NE
247 mins	2026-02-04 05:45:54.989Z	223.724° SW	2026-02-04 08:59:54.989Z	334.079° NNW	38.614°	2026-02-04 09:52:54.989Z	64.103° ENE
49 mins	2026-02-04 14:44:54.989Z	329.284° NNW	2026-02-04 15:33:54.989Z	275.13° WNW	36.116°	2026-02-04 15:33:54.989Z	275.13° WNW

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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), 29680 on other resources

View SL-12 R/B(AUX MOTOR), 29680 on Heavens-Above

View SL-12 R/B(AUX MOTOR), 29680 on Keep Track

View SL-12 R/B(AUX MOTOR), 29680 on Celestrak

View SL-12 R/B(AUX MOTOR), 29680 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), 29680

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-02-02T08:54:21.965Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #62 in the year 2006 (2006-12-25 UTC)

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

Co-orbital & Co-planar RSOs

Check out SL-12 R/B(AUX MOTOR), 29680 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago