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: 16 hours ago

TLE from 16 hours ago

0 SL-16 R/B DEB
1 49050U 92093LX  26037.08891572  .00026480  00000-0  12261-1 0  9992
2 49050  71.0164  69.5748 0013121 302.3547  57.6308 14.20636522 14566

Epoch: 2026-02-06T02:08Z

TLE epoch observation values (Epoch: 2026-02-06T02:08:02.318Z)

Latitude

-0°

Longitude

-98.66666°

Altitude

820.558 km

Speed

7.446 km/s

True Right ascension

04h 38m 17s

True Declination

0° 00' 00"

Sunlit

Object was in daylight 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

20:37:36

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

830.565 km

Perigee altitude

811.673 km

Semi-major axis

7,199.256 km

Eccentricity

0.00131

Inclination

71.0164°

RAAN

69.5748°

Arg. of periapsis

302.3547°

True anomaly

57.7579°

Mean anomaly

57.6308°

Eccentric anomaly

57.69434°

Mean motion

3.55314 °/min

Orbital period

101.32 mins

BSTAR

0.012261

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

SL-16 DEB, 22484 (Decayed)

SL-16 DEB, 22846 (Decayed)

SL-16 DEB, 39723

SL-16 DEB, 22492 (Decayed)

SL-16 DEB, 22508 (Decayed)

SL-16 DEB, 22345 (Decayed)

SL-16 DEB, 22401 (Decayed)

SL-16 DEB, 22555 (Decayed)

SL-16 DEB, 22420 (Decayed)

SL-16 DEB, 22389 (Decayed)

SL-16 DEB, 39841 (Decayed)

SL-16 DEB, 26979 (Decayed)

SL-16 DEB, 22413 (Decayed)

SL-16 DEB, 22291

SL-16 DEB, 22353

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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	2026-02-07 01:55:27.872Z	129.11° SE	2026-02-07 01:58:27.872Z	95.413° ESE	14.176°	2026-02-07 02:00:27.872Z	72.553° E
9 mins	2026-02-07 03:37:27.872Z	214.144° SW	2026-02-07 03:41:27.872Z	315.432° NNW	42.959°	2026-02-07 03:46:27.872Z	18.248° NNE
9 mins	2026-02-07 12:29:27.872Z	352.95° N	2026-02-07 12:33:27.872Z	53.733° ENE	35.724°	2026-02-07 12:38:27.872Z	132.907° SE
6 mins	2026-02-07 14:14:27.872Z	294.197° NW	2026-02-07 14:17:27.872Z	251.043° W	21.327°	2026-02-07 14:20:27.872Z	214.014° SW

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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: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2026-02-06T02:08:02.318Z)

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: 16 hours ago