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

Orbit data source: Space-Track

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

https://www.satcat.com/sats-embedded/29682?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29682, 2006-062H

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)

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, 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 29682U 06062H   25181.23298884  .00000069  00000-0  53921-4 0  9991
2 29682  65.1710 141.2080 5551988 269.4661  30.1760  4.25379863286606

Epoch: 2025-06-30T05:35Z

TLE epoch observation values (Epoch: 2025-06-30T05:35:30.235Z)

Latitude

-0.00005°

Longitude

138.7827°

Altitude

4,823.4 km

Speed

6.812 km/s

True Right ascension

09h 24m 49s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

63.51009°

Longitude

-154.07409°

Altitude

18,274.215 km

Speed

2.754 km/s

Apparent Right ascension

14h 26m 04s

Apparent Declination

49° 09' 32"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

03:40:34

Azimuth

12.054° NNE

Elevation

0.58°

Doppler factor

Orbital elements

Apogee altitude

18,642.968 km

Perigee altitude

778.13 km

Semi-major axis

16,088.686 km

Eccentricity

0.5552

Inclination

65.171°

RAAN

141.208°

Arg. of periapsis

269.4661°

True anomaly

Unknown

Mean anomaly

30.176°

Eccentric anomaly

Unknown

Mean motion

1.06356 °/min

Orbital period

338.49 mins

BSTAR

0.000053921

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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), 29680

SL-12 DEB, 41809 (Decayed)

SL-12 DEB, 41810

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.
185 mins	2025-07-02 19:41:16.206Z	135.134° SSE	2025-07-02 20:28:16.206Z	68.802° E	34.849°	2025-07-02 22:46:16.206Z	31.511° NE
261 mins	2025-07-03 01:29:16.206Z	256.314° W	2025-07-03 03:59:16.206Z	10.468° NNE	39.917°	2025-07-03 05:50:16.206Z	106.274° ESE
179 mins	2025-07-03 08:37:16.206Z	329.371° NNW	2025-07-03 10:50:16.206Z	292.465° WNW	33.757°	2025-07-03 11:36:16.206Z	227.657° WSW

Authenticating...

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Check out SL-12 R/B(AUX MOTOR), 29682 on other resources

View SL-12 R/B(AUX MOTOR), 29682 on Heavens-Above

View SL-12 R/B(AUX MOTOR), 29682 on Keep Track

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

View SL-12 R/B(AUX MOTOR), 29682 on Gunter's Space Page

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