SL-16 DEB, 44574

Orbit data source: Space-Track

SL-16 DEB, 44574 is space debris in LEO originally from a launch on Fri, 25 Dec 1992 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/44574?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

44574, 1992-093LW

Orbit

LEO

Last TLE update

11 hours ago

Origin

Russian Strategic Rocket Forces (CIS)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1992-12-25 (33 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 11 hours ago

0 SL-16 DEB
1 44574U 92093LW  25224.61937006  .00008864  00000-0  23236-2 0  9998
2 44574  71.1203  50.7624 0089289 142.4062 281.6453 14.47089889610014

Epoch: 2025-08-12T14:51Z

TLE epoch observation values (Epoch: 2025-08-12T14:51:53.573Z)

Latitude

57.6158°

Longitude

-101.08707°

Altitude

732.051 km

Speed

7.501 km/s

True Right ascension

05h 32m 46s

True Declination

57° 27' 34"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-34.81936°

Longitude

59.18852°

Altitude

730.985 km

Speed

7.497 km/s

Apparent Right ascension

17h 33m 44s

Apparent Declination

-82° 51' 14"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

15:57:37

Azimuth

176.524° S

Elevation

-33.335°

Doppler factor

Orbital elements

Apogee altitude

796.546 km

Perigee altitude

669.555 km

Semi-major axis

7,111.187 km

Eccentricity

0.00893

Inclination

71.1203°

RAAN

50.7624°

Arg. of periapsis

142.4062°

True anomaly

280.64097°

Mean anomaly

281.6453°

Eccentric anomaly

281.14336°

Mean motion

3.61934 °/min

Orbital period

99.47 mins

BSTAR

0.0023236

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Other satellites on launch #93 in the year 1992 (1992-12-25 UTC)

SL-16 DEB, 22345 (Decayed)

SL-16 DEB, 22346 (Decayed)

SL-16 DEB Visibility forecast

Observer location: undefined°, undefined°
Set Observer location

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.
8 mins	2025-08-13 13:56:06.810Z	208.196° SW	2025-08-13 14:00:06.810Z	311.56° NW	44.237°	2025-08-13 14:04:06.810Z	19.016° NNE
7 mins	2025-08-13 22:39:06.810Z	6.59° NNE	2025-08-13 22:42:06.810Z	57.081° ENE	25.516°	2025-08-13 22:46:06.810Z	117.899° SE
6 mins	2025-08-14 00:21:06.810Z	303.071° NW	2025-08-14 00:24:06.810Z	247.874° W	25.183°	2025-08-14 00:27:06.810Z	201.945° SSW

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

Click to sort rows by RSO header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Type header in ascending order	Click to sort rows by Inclination Δ header in ascending order	Click to sort rows by RAAN Δ header in ascending order	Click to sort rows by Coplanar Angle header in ascending order	Click to sort rows by SMA Δ header in ascending order	Click to sort rows by Orbital period header in ascending order	Click to sort rows by <5km Md TCA header in ascending order

Authenticating...

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Check out SL-16 DEB, 44574 on other resources

View SL-16 DEB, 44574 on Heavens-Above

View SL-16 DEB, 44574 on Keep Track

View SL-16 DEB, 44574 on Celestrak

View SL-16 DEB, 44574 on Gunter's Space Page

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