SL-16 R/B DEB, 49050

Orbit data source: Space-Track

SL-16 R/B DEB, 49050 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/49050?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

49050, 1992-093LX

Orbit

LEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

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 shape, 0.1 m

Radar Cross Section

RCS unknown

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 SL-16 R/B DEB
1 49050U 92093LX  26132.37026870  .00008290  00000-0  36129-2 0  9990
2 49050  71.0131 227.1362 0008442 176.8220 183.2962 14.24167493 28114

Epoch: 2026-05-12T08:53Z

TLE epoch observation values (Epoch: 2026-05-12T08:53:11.215Z)

Latitude

-0.0001°

Longitude

-136.30618°

Altitude

819.765 km

Speed

7.44 km/s

True Right ascension

15h 08m 32s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

18:39:28

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

815.275 km

Perigee altitude

803.14 km

Semi-major axis

7,187.345 km

Eccentricity

0.00084

Inclination

71.0131°

RAAN

227.1362°

Arg. of periapsis

176.822°

True anomaly

183.29064°

Mean anomaly

183.2962°

Eccentric anomaly

183.29342°

Mean motion

3.56197 °/min

Orbital period

101.07 mins

BSTAR

0.0036129

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

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SL-16 R/B DEB 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.
5 mins	2026-05-13 15:47:11.629Z	21.218° NNE	2026-05-13 15:49:11.629Z	45.073° ENE	15.443°	2026-05-13 15:52:11.629Z	81.555° E
9 mins	2026-05-13 17:29:11.629Z	332.833° NNW	2026-05-13 17:33:11.629Z	291.561° WNW	43.529°	2026-05-13 17:38:11.629Z	165.287° S
7 mins	2026-05-14 06:32:11.629Z	148.074° SSE	2026-05-14 06:35:11.629Z	100.621° ESE	25.905°	2026-05-14 06:39:11.629Z	48.17° ENE
8 mins	2026-05-14 08:15:11.629Z	246.395° WSW	2026-05-14 08:18:11.629Z	298.446° NW	30.829°	2026-05-14 08:23:11.629Z	6.806° NNE

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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-16 R/B DEB, 49050 on other resources

View SL-16 R/B DEB, 49050 on Heavens-Above

View SL-16 R/B DEB, 49050 on Keep Track

View SL-16 R/B DEB, 49050 on Celestrak

View SL-16 R/B DEB, 49050 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-16 R/B DEB, 49050

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-05-12T08:53:11.215Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

SL-16 R/B DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-16 R/B DEB, 49050 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago