SL-16 R/B, 22566

Orbit data source: Space-Track

SL-16 R/B, 22566 is space debris in LEO originally from a launch on Fri, 26 Mar 1993 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.

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https://www.satcat.com/sats-embedded/22566?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

22566, 1993-016B

Orbit

LEO

Country

CIS

Related business

Russian Space Forces (RU)

Manufacturer

Yuzhnoe

Mission

Spacecraft

Bus & Motor

11S772, Unknown motor

Mass

9,000 kg wet, 9,000 kg dry

Launch date (UTC)

1993-03-26 (33 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 5.2 m

Radar Cross Section

37.829 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago

0 SL-16 R/B
1 22566U 93016B   25353.20754429  .00000250  00000-0  15270-3 0  9996
2 22566  71.0079  24.2194 0008012  85.0882 275.1155 14.15288648690784

Epoch: 2025-12-19T04:58Z

TLE epoch observation values (Epoch: 2025-12-19T04:58:51.826Z)

Latitude

-0.00007°

Longitude

-138.54857°

Altitude

843.22 km

Speed

7.432 km/s

True Right ascension

01h 36m 52s

True Declination

0° 00' 00"

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

19:30:51

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

845.037 km

Perigee altitude

833.472 km

Semi-major axis

7,217.391 km

Eccentricity

0.0008

Inclination

71.0079°

RAAN

24.2194°

Arg. of periapsis

85.0882°

True anomaly

275.02405°

Mean anomaly

275.1155°

Eccentric anomaly

275.06977°

Mean motion

3.53975 °/min

Orbital period

101.7 mins

BSTAR

0.0001527

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Other satellites on launch #16 in the year 1993 (1993-03-26 UTC)

SL-16 DEB, 29099 (Decayed)

SL-16 DEB, 39897 (Decayed)

SL-16 DEB, 42246

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SL-16 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.
10 mins	2025-12-20 03:08:33.698Z	182.087° SSW	2025-12-20 03:13:33.698Z	105.072° ESE	38.797°	2025-12-20 03:18:33.698Z	33.416° NE
7 mins	2025-12-20 04:54:33.698Z	263.374° W	2025-12-20 04:57:33.698Z	301.496° NW	20.844°	2025-12-20 05:01:33.698Z	352.315° N
7 mins	2025-12-20 12:04:33.698Z	13.107° NNE	2025-12-20 12:07:33.698Z	53.931° ENE	21.978°	2025-12-20 12:11:33.698Z	104.058° ESE
9 mins	2025-12-20 13:47:33.698Z	322.748° NNW	2025-12-20 13:51:33.698Z	265.098° W	37.13°	2025-12-20 13:56:33.698Z	181.27° 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-16 R/B, 22566 on other resources

View SL-16 R/B, 22566 on Heavens-Above

View SL-16 R/B, 22566 on Keep Track

View SL-16 R/B, 22566 on Celestrak

View SL-16 R/B, 22566 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-16 R/B, 22566

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2025-12-19T04:58:51.826Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #16 in the year 1993 (1993-03-26 UTC)

SL-16 R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-16 R/B, 22566 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 16 hours ago