SL-6 DEB, 48265

Orbit data source: Space-Track

SL-6 DEB, 48265 is space debris in HEO originally from a launch on Wed, 23 Dec 1981 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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https://www.satcat.com/sats-embedded/48265?theme=dark&initialShowStats=false

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Identifier

48265, 1981-123E

Orbit

HEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

RKKE

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1981-12-23 (44 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 1.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

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

TLE from 1 week ago

0 SL-6 DEB
1 48265U 81123E   26164.30442741 -.00000013  00000-0  00000-0 0  9999
2 48265  62.3129  63.4954 7129285 276.9657 341.5643  2.19416933100642

Epoch: 2026-06-13T07:18Z

TLE epoch observation values (Epoch: 2026-06-13T07:18:22.528Z)

Latitude

-0.52819°

Longitude

-127.40287°

Altitude

7,013.501 km

Speed

6.603 km/s

True Right ascension

16h 15m 14s

True Declination

0° 31' 35"

Sunlit

Object was in partial 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

21:25:42

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

36,471.351 km

Perigee altitude

803.054 km

Semi-major axis

25,015.339 km

Eccentricity

0.71293

Inclination

62.3129°

RAAN

63.4954°

Arg. of periapsis

276.9657°

True anomaly

263.21914°

Mean anomaly

341.5643°

Eccentric anomaly

310.50632°

Mean motion

0.54857 °/min

Orbital period

656.25 mins

BSTAR

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Other satellites on launch #123 in the year 1981 (1981-12-23 UTC)

SL-6 R/B(1), 13013 (Decayed)

MOLNIYA 1-52, 13012

SL-6 R/B(2), 13016

SL-6 PLAT, 13014 (Decayed)

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SL-6 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.
286 mins	2026-06-22 12:52:42.196Z	36.44° NE	2026-06-22 14:53:42.196Z	26.931° NE	14.756°	2026-06-22 17:38:42.196Z	30.692° NE
571 mins	2026-06-22 22:20:42.196Z	275.34° WNW	2026-06-23 04:16:42.196Z	317.278° NNW	37.733°	2026-06-23 07:51:42.196Z	241.144° WSW

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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-6 DEB, 48265 on other resources

View SL-6 DEB, 48265 on Heavens-Above

View SL-6 DEB, 48265 on Keep Track

View SL-6 DEB, 48265 on Celestrak

View SL-6 DEB, 48265 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-6 DEB, 48265

Orbit data source: Space-Track

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

TLE from 1 week ago

TLE epoch observation values (Epoch: 2026-06-13T07:18:22.528Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #123 in the year 1981 (1981-12-23 UTC)

SL-6 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-6 DEB, 48265 on other resources

Documentation

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