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SL-12 DEB, 19753

Orbit data source: Space-Track

SL-12 DEB, 19753 is space debris in MEO originally from a launch on Tue, 10 Jan 1989 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/19753?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/19753?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

19753, 1989-001E

Orbit

MEO

Last TLE update

12 hours ago

Origin

Federal Space Agency of Russia (Roscosmos) (CIS)

Manufacturer

NPO PM

Mission

Spacecraft

Bus & Motor

ETALON ADAPTER, Unknown motor

Mass

Unknown

Launch date (UTC)

1989-01-10 (36 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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 12 hours ago

0 SL-12 DEB
1 19753U 89001E   25183.63143245 -.00000048  00000-0  00000-0 0  9993
2 19753  64.7427  84.1400 0024013 215.7088 336.7723  2.13160780284233

Epoch: 2025-07-02T15:09Z

TLE epoch observation values (Epoch: 2025-07-02T15:09:15.763Z)

Latitude

-11.21352°

Longitude

121.27907°

Altitude

19,071.674 km

Speed

3.962 km/s

True Right ascension

17h 58m 01s

True Declination

-11° 11' 43"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-32.91735°

Longitude

133.64584°

Altitude

19,074.577 km

Speed

3.962 km/s

Apparent Right ascension

19h 37m 22s

Apparent Declination

-42° 55' 38"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

14:55:41

Azimuth

134.578° SE

Elevation

-14.408°

Doppler factor

1

Orbital elements

Apogee altitude

19,186.062 km

Perigee altitude

19,063.581 km

Semi-major axis

25,502.959 km

Eccentricity

0.0024

Inclination

64.7427°

RAAN

84.14°

Arg. of periapsis

215.7088°

True anomaly

Unknown

Mean anomaly

336.7723°

Eccentric anomaly

Unknown

Mean motion

0.53291 °/min

Orbital period

675.53 mins

BSTAR

0

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Other satellites on launch #1 in the year 1989 (1989-01-10 UTC)

COSMOS 1987 (GLONASS), 19749

COSMOS 1988 (GLONASS), 19750

COSMOS 1989 (ETALON 1), 19751

SL-12 R/B(1), 19752 (Decayed)

SL-12 R/B(2), 19754

SL-12 R/B(AUX MOTOR), 19755

SL-12 R/B(AUX MOTOR), 19856

SL-12 DEB, 25797 (Decayed)

SL-12 DEB, 25798

SL-12 DEB, 25799 (Decayed)

SL-12 DEB, 26046 (Decayed)

SL-12 DEB, 26047 (Decayed)

SL-12 DEB, 26813

SL-12 DEB, 26814 (Decayed)

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.
333 mins	2025-07-03 18:04:32.601Z	196.036° SSW	2025-07-03 20:28:32.601Z	295.983° NW	44.137°	2025-07-03 23:37:32.601Z	75.165° E

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Check out SL-12 DEB, 19753 on other resources

View SL-12 DEB, 19753 on Heavens-Above

View SL-12 DEB, 19753 on Keep Track

View SL-12 DEB, 19753 on Celestrak

View SL-12 DEB, 19753 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

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