SL-12 R/B(2), 13630

Orbit data source: Space-Track

SL-12 R/B(2), 13630 is space debris in GEO originally from a launch on Wed, 20 Oct 1982 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

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Iframe URL

https://www.satcat.com/sats-embedded/13630?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

13630, 1982-103E

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)

1982-10-20 (43 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

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Last TLE update: 10 hours ago

TLE from 10 hours ago

0 SL-12 R/B(2)
1 13630U 82103E   26083.50659155 -.00000327  00000-0  00000+0 0  9994
2 13630   7.4835 302.3737 0010682 189.5619   5.4640  1.00350339120650

Epoch: 2026-03-24T12:09Z

TLE epoch observation values (Epoch: 2026-03-24T12:09:29.509Z)

Latitude

-1.95145°

Longitude

132.96264°

Altitude

35,719.589 km

Speed

3.079 km/s

True Right ascension

09h 09m 16s

True Declination

-1° 56' 58"

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

03:07:02

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,810.65 km

Perigee altitude

35,720.614 km

Semi-major axis

42,143.769 km

Eccentricity

0.00107

Inclination

7.4835°

RAAN

302.3737°

Arg. of periapsis

189.5619°

True anomaly

5.47567°

Mean anomaly

5.464°

Eccentric anomaly

5.46983°

Mean motion

0.25087 °/min

Orbital period

1,435.02 mins

BSTAR

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Other satellites on launch #103 in the year 1982 (1982-10-20 UTC)

GORIZONT 6, 13624

SL-12 R/B(1), 13625 (Decayed)

SL-12 PLAT, 13626 (Decayed)

SL-12 R/B(AUX MOTOR), 13644 (Decayed)

SL-12 R/B(AUX MOTOR), 13629 (Decayed)

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SL-12 R/B(2) Visibility

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13630 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), 13630 on other resources

View SL-12 R/B(2), 13630 on Heavens-Above

View SL-12 R/B(2), 13630 on Keep Track

View SL-12 R/B(2), 13630 on Celestrak

View SL-12 R/B(2), 13630 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), 13630

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: 2026-03-24T12:09:29.509Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #103 in the year 1982 (1982-10-20 UTC)

SL-12 R/B(2) Visibility

13630 neighbors

Co-orbital & Co-planar RSOs

Check out SL-12 R/B(2), 13630 on other resources

Documentation

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