SL-12 R/B(2), 21019

Orbit data source: Space-Track

SL-12 R/B(2), 21019 is space debris in GEO originally from a launch on Thu, 20 Dec 1990 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.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/21019?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/21019?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

21019, 1990-112D

Orbit

GEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

NPO Energiya

Mission

Spacecraft

Bus & Motor

BLOK DM, Unknown motor

Mass

2,440 kg wet, 2,440 kg dry

Launch date (UTC)

1990-12-20 (35 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 3.1 m

Radar Cross Section

23.597 m², Large (>1 m²)

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Last TLE update: 2 days ago

TLE from 2 days ago

0 SL-12 R/B(2)
1 21019U 90112D   25303.89211016  .00000078  00000-0  00000+0 0  9991
2 21019  13.1027 339.6815 0027017 181.2213 220.4049  1.00029956117641

Epoch: 2025-10-30T21:24Z

TLE epoch observation values (Epoch: 2025-10-30T21:24:38.317Z)

Latitude

8.63359°

Longitude

19.72906°

Altitude

35,940.722 km

Speed

3.066 km/s

True Right ascension

01h 21m 19s

True Declination

8° 37' 30"

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

11:57:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,969.616 km

Perigee altitude

35,741.411 km

Semi-major axis

42,233.65 km

Eccentricity

0.0027

Inclination

13.1027°

RAAN

339.6815°

Arg. of periapsis

181.2213°

True anomaly

220.20474°

Mean anomaly

220.4049°

Eccentric anomaly

220.30477°

Mean motion

0.25007 °/min

Orbital period

1,439.62 mins

BSTAR

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Other satellites on launch #112 in the year 1990 (1990-12-20 UTC)

SL-12 PLAT, 21018 (Decayed)

SL-12 R/B(AUX MOTOR), 21025 (Decayed)

RADUGA 26, 21016

SL-12 R/B(AUX MOTOR), 21024 (Decayed)

SL-12 R/B(1), 21017 (Decayed)

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SL-12 R/B(2) Visibility

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21019 neighbors

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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-12 R/B(2), 21019 on other resources

View SL-12 R/B(2), 21019 on Heavens-Above

View SL-12 R/B(2), 21019 on Keep Track

View SL-12 R/B(2), 21019 on Celestrak

View SL-12 R/B(2), 21019 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-12 R/B(2), 21019

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2025-10-30T21:24:38.317Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #112 in the year 1990 (1990-12-20 UTC)

SL-12 R/B(2) Visibility

21019 neighbors

Co-orbital & Co-planar RSOs

Check out SL-12 R/B(2), 21019 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago