SL-6 R/B(2), 23645

Orbit data source: Space-Track

SL-6 R/B(2), 23645 is space debris originally from a launch on Wed, 09 Aug 1995 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/23645?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

23645, 1995-042D

Orbit

Molniya

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

RKKE

Mission

Spacecraft

Bus & Motor

BLOK-L, Unknown motor

Mass

900 kg wet, 900 kg dry

Launch date (UTC)

1995-08-09 (31 years ago)

Launch vehicle

Unknown

Launch site

Plesetsk Missile And Space Complex (PKMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, Unknown HBR

Radar Cross Section

7.275 m², Large (>1 m²)

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

TLE from 2 weeks ago

0 SL-6 R/B(2)
1 23645U 95042D   26152.02337491  .00000654  00000-0  00000-0 0  9990
2 23645  64.8395 316.1022 7012460 271.1641  16.3599  1.99195229221605

Epoch: 2026-06-01T00:33Z

TLE epoch observation values (Epoch: 2026-06-01T00:33:39.592Z)

Latitude

0.00056°

Longitude

58.11776°

Altitude

6,970.623 km

Speed

6.692 km/s

True Right ascension

21h 04m 11s

True Declination

0° 00' 02"

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

11:19:28

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

39,012.502 km

Perigee altitude

1,592.865 km

Semi-major axis

26,680.821 km

Eccentricity

0.70125

Inclination

64.8395°

RAAN

316.1022°

Arg. of periapsis

271.1641°

True anomaly

88.68465°

Mean anomaly

16.3599°

Eccentric anomaly

44.54267°

Mean motion

0.49802 °/min

Orbital period

722.87 mins

BSTAR

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Computing Atmospheric mass density...

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Other satellites on launch #42 in the year 1995 (1995-08-09 UTC)

SL-6 PLAT, 23644 (Decayed)

SL-6 R/B(1), 23643 (Decayed)

MOLNIYA 3-47, 23642

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SL-6 R/B(2) 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.
98 mins	2026-06-13 06:01:30.272Z	17.28° NNE	2026-06-13 06:49:30.272Z	16.067° NNE	10.692°	2026-06-13 07:39:30.272Z	15.526° NNE
650 mins	2026-06-13 13:52:30.272Z	245.294° WSW	2026-06-13 22:22:30.272Z	310.245° NW	39.711°	2026-06-14 00:42:30.272Z	223.218° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out SL-6 R/B(2), 23645 on other resources

View SL-6 R/B(2), 23645 on Heavens-Above

View SL-6 R/B(2), 23645 on Keep Track

View SL-6 R/B(2), 23645 on Celestrak

View SL-6 R/B(2), 23645 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 R/B(2), 23645

Orbit data source: Space-Track

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

TLE from 2 weeks ago

TLE epoch observation values (Epoch: 2026-06-01T00:33:39.592Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #42 in the year 1995 (1995-08-09 UTC)

SL-6 R/B(2) Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-6 R/B(2), 23645 on other resources

Documentation

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