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: 3 days ago

TLE from 3 days ago

0 SL-12 R/B(AUX MOTOR)
1 29680U 06062G   25253.95573091 -.00000014  00000-0 -22816-5 0  9996
2 29680  65.1447 135.9173 5688076 224.5988  72.4181  4.25851591188540

Epoch: 2025-09-10T22:56Z

TLE epoch observation values (Epoch: 2025-09-10T22:56:15.15Z)

Latitude

0.00003°

Longitude

161.64253°

Altitude

11,909.37 km

Speed

4.337 km/s

True Right ascension

09h 03m 43s

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

09:48:12

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

18,843.215 km

Perigee altitude

554.042 km

Semi-major axis

16,076.765 km

Eccentricity

0.56881

Inclination

65.1447°

RAAN

135.9173°

Arg. of periapsis

224.5988°

True anomaly

135.47754°

Mean anomaly

72.4181°

Eccentric anomaly

104.03542°

Mean motion

1.06474 °/min

Orbital period

338.11 mins

BSTAR

-0.0000022816

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

COSMOS 2425 (GLONASS), 29670

COSMOS 2426 (GLONASS), 29671

COSMOS 2424 (GLONASS), 29672

SL-12 R/B(2), 29673

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

SL-12 PLAT, 29675 (Decayed)

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

SL-12 DEB, 41809 (Decayed)

SL-12 DEB, 41810

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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.
253 mins	2025-09-13 18:21:53.166Z	219.262° SW	2025-09-13 21:03:53.166Z	314.153° NW	40.015°	2025-09-13 22:34:53.166Z	63.502° ENE
81 mins	2025-09-14 03:07:53.166Z	327.743° NNW	2025-09-14 04:16:53.166Z	269.407° W	39.277°	2025-09-14 04:28:53.166Z	191.267° SSW
152 mins	2025-09-14 12:13:53.166Z	83.492° E	2025-09-14 13:41:53.166Z	54.252° ENE	23.591°	2025-09-14 14:45:53.166Z	28.31° NE
28 mins	2025-09-14 16:48:53.166Z	195.157° SSW	2025-09-14 17:16:53.166Z	198.735° SSW	32.796°	2025-09-14 17:16:53.166Z	198.735° SSW

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), 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: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2025-09-10T22:56:15.15Z)

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: 3 days ago