SL-8 R/B, 3048

Orbit data source: Space-Track

SL-8 R/B, 3048 is space debris in LEO originally from a launch on Thu, 23 Nov 1967 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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/3048?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

3048, 1967-116B

Orbit

LEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

Yuzhnoe

Mission

Spacecraft

Bus & Motor

S3, Unknown motor

Mass

1,434 kg wet, 1,434 kg dry

Launch date (UTC)

1967-11-23 (58 years ago)

Launch vehicle

Unknown

Launch site

Plesetsk Missile And Space Complex (PKMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago

0 SL-8 R/B
1  3048U 67116B   26004.89530828  .00001000  00000-0  20004-3 0  9991
2  3048  74.0061 163.1501 0007889 311.7608 161.6209 14.63203311 82155

Epoch: 2026-01-04T21:29Z

TLE epoch observation values (Epoch: 2026-01-04T21:29:14.635Z)

Latitude

62.00864°

Longitude

-116.09799°

Altitude

698.407 km

Speed

7.51 km/s

True Right ascension

20h 42m 51s

True Declination

61° 51' 53"

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

02:54:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

686.015 km

Perigee altitude

674.878 km

Semi-major axis

7,058.583 km

Eccentricity

0.00079

Inclination

74.0061°

RAAN

163.1501°

Arg. of periapsis

311.7608°

True anomaly

161.64938°

Mean anomaly

161.6209°

Eccentric anomaly

161.63514°

Mean motion

3.65988 °/min

Orbital period

98.36 mins

BSTAR

0.00020004

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Other satellites on launch #116 in the year 1967 (1967-11-23 UTC)

COSMOS 192 DEB, 35876 (Decayed)

COSMOS 192 DEB, 35878 (Decayed)

COSMOS 192, 3047

COSMOS 192 DEB, 35877 (Decayed)

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SL-8 R/B 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.
8 mins	2026-01-05 11:52:32.148Z	209.804° SW	2026-01-05 11:55:32.148Z	255.242° W	41.858°	2026-01-05 12:00:32.148Z	13.504° NNE
5 mins	2026-01-05 20:30:32.148Z	27.138° NE	2026-01-05 20:32:32.148Z	56.011° ENE	17.094°	2026-01-05 20:35:32.148Z	97.609° ESE
7 mins	2026-01-05 22:10:32.148Z	320.044° NNW	2026-01-05 22:13:32.148Z	241.647° WSW	36.826°	2026-01-05 22:17:32.148Z	182.675° SSW

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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-8 R/B, 3048 on other resources

View SL-8 R/B, 3048 on Heavens-Above

View SL-8 R/B, 3048 on Keep Track

View SL-8 R/B, 3048 on Celestrak

View SL-8 R/B, 3048 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-8 R/B, 3048

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 5 hours ago

TLE from 5 hours ago

TLE epoch observation values (Epoch: 2026-01-04T21:29:14.635Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #116 in the year 1967 (1967-11-23 UTC)

SL-8 R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-8 R/B, 3048 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 5 hours ago