SL-12 DEB, 41768

Orbit data source: Space-Track

SL-12 DEB, 41768 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/41768?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41768, 2006-062J

Orbit

HEO

Last TLE update

3 days ago

Origin

Russian Space Forces (CIS)

Manufacturer

RKKE

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

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

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 3 days ago

0 SL-12 DEB
1 41768U 06062J   25180.42761357 -.00000600  00000-0 -43824-2 0  9992
2 41768  64.7039  60.0697 5453959 295.7713  18.5723  4.48777376139809

Epoch: 2025-06-29T10:15Z

TLE epoch observation values (Epoch: 2025-06-29T10:15:45.812Z)

Latitude

-0.00011°

Longitude

-11.60836°

Altitude

2,451.818 km

Speed

8.039 km/s

True Right ascension

04h 00m 20s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

58.80451°

Longitude

115.96228°

Altitude

17,426.82 km

Speed

2.799 km/s

Apparent Right ascension

13h 11m 38s

Apparent Declination

44° 33' 42"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

02:58:11

Azimuth

18.645° NNE

Elevation

-2.19°

Doppler factor

Orbital elements

Apogee altitude

17,613.364 km

Perigee altitude

679.365 km

Semi-major axis

15,524.502 km

Eccentricity

0.5454

Inclination

64.7039°

RAAN

60.0697°

Arg. of periapsis

295.7713°

True anomaly

Unknown

Mean anomaly

18.5723°

Eccentric anomaly

Unknown

Mean motion

1.12206 °/min

Orbital period

320.84 mins

BSTAR

-0.0043824

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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 R/B(AUX MOTOR), 29682

SL-12 DEB, 41809 (Decayed)

SL-12 DEB, 41810

SL-12 DEB 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.
211 mins	2025-07-02 18:34:00.949Z	231.824° WSW	2025-07-02 19:00:00.949Z	313.944° NW	43.346°	2025-07-02 22:05:00.949Z	74.245° E
226 mins	2025-07-03 00:31:00.949Z	315.032° NNW	2025-07-03 03:01:00.949Z	268.213° W	44.825°	2025-07-03 04:17:00.949Z	176.844° S
90 mins	2025-07-03 06:52:00.949Z	332.47° NNW	2025-07-03 07:35:00.949Z	318.003° NNW	14.515°	2025-07-03 08:22:00.949Z	300.761° NW

Authenticating...

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Check out SL-12 DEB, 41768 on other resources

View SL-12 DEB, 41768 on Heavens-Above

View SL-12 DEB, 41768 on Keep Track

View SL-12 DEB, 41768 on Celestrak

View SL-12 DEB, 41768 on Gunter's Space Page

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