SL-8 R/B, 15006

Orbit data source: Space-Track

SL-8 R/B, 15006 is space debris in LEO originally from a launch on Mon, 28 May 1984 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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https://www.satcat.com/sats-embedded/15006?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

15006, 1984-052J

Orbit

LEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

Omsk Av. Zav.

Mission

Spacecraft

Bus & Motor

S3, Unknown motor

Mass

1,434 kg wet, 1,434 kg dry

Launch date (UTC)

1984-05-28 (42 years ago)

Launch vehicle

Unknown

Launch site

Plesetsk Missile And Space Complex (PKMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

CYL, 1.1 m

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago

0 SL-8 R/B
1 15006U 84052J   26277.57564840 -.00000100  00000-0 -77199-3 0  9993
2 15006  74.0100  75.7886 0132134 126.9730 299.8666 12.23751866892016

Epoch: 2026-10-04T13:48Z

TLE epoch observation values (Epoch: 2026-10-04T13:48:56.021Z)

Latitude

61.12346°

Longitude

-113.57623°

Altitude

1,535.01 km

Speed

7.127 km/s

True Right ascension

07h 07m 41s

True Declination

60° 59' 32"

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

18:09:30

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,679.184 km

Perigee altitude

1,469.032 km

Semi-major axis

7,952.245 km

Eccentricity

0.01321

Inclination

74.01°

RAAN

75.7886°

Arg. of periapsis

126.973°

True anomaly

298.54279°

Mean anomaly

299.8666°

Eccentric anomaly

299.20577°

Mean motion

3.06061 °/min

Orbital period

117.62 mins

BSTAR

-0.00077199

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Other satellites on launch #52 in the year 1984 (1984-05-28 UTC)

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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.
16 mins	2026-10-05 11:07:11.622Z	173.313° S	2026-10-05 11:15:11.622Z	105.044° ESE	54.355°	2026-10-05 11:23:11.622Z	29.294° NE
14 mins	2026-10-05 13:09:11.622Z	243.368° WSW	2026-10-05 13:16:11.622Z	306.424° NW	35.973°	2026-10-05 13:23:11.622Z	3.093° NNE
6 mins	2026-10-05 19:30:11.622Z	24.223° NE	2026-10-05 19:33:11.622Z	46.532° ENE	14.348°	2026-10-05 19:36:11.622Z	68.15° E
15 mins	2026-10-05 21:28:11.622Z	349.514° N	2026-10-05 21:35:11.622Z	77.581° E	64.194°	2026-10-05 21:43:11.622Z	148.271° SSE
11 mins	2026-10-05 23:29:11.622Z	309.793° NW	2026-10-05 23:34:11.622Z	267.155° W	26.223°	2026-10-05 23:40:11.622Z	218.759° 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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Check out SL-8 R/B, 15006 on other resources

View SL-8 R/B, 15006 on Heavens-Above

View SL-8 R/B, 15006 on Keep Track

View SL-8 R/B, 15006 on Celestrak

View SL-8 R/B, 15006 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, 15006

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-10-04T13:48:56.021Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #52 in the year 1984 (1984-05-28 UTC)

SL-8 R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-8 R/B, 15006 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago