SL-16 DEB, 22816

Orbit data source: Space-Track

SL-16 DEB, 22816 is space debris in LEO originally from a launch on Fri, 25 Dec 1992 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/22816?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

22816, 1992-093JC

Orbit

LEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1992-12-25 (33 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago

0 SL-16 DEB
1 22816U 92093JC  26171.19250984  .00028906  00000-0  33228-2 0  9992
2 22816  71.4417  96.9866 0035135 316.6321  43.2077 14.85237747710164

Epoch: 2026-06-20T04:37Z

TLE epoch observation values (Epoch: 2026-06-20T04:37:12.850Z)

Latitude

-0.00003°

Longitude

119.27239°

Altitude

597.483 km

Speed

7.571 km/s

True Right ascension

06h 27m 56s

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

10:02:26

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

635.207 km

Perigee altitude

586.097 km

Semi-major axis

6,988.789 km

Eccentricity

0.00351

Inclination

71.4417°

RAAN

96.9866°

Arg. of periapsis

316.6321°

True anomaly

43.48423°

Mean anomaly

43.2077°

Eccentric anomaly

43.34588°

Mean motion

3.71484 °/min

Orbital period

96.91 mins

BSTAR

0.0033228

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Other satellites on launch #93 in the year 1992 (1992-12-25 UTC)

SL-16 DEB, 22501 (Decayed)

SL-16 DEB, 22346 (Decayed)

SL-16 DEB, 22464 (Decayed)

SL-16 DEB, 22360 (Decayed)

SL-16 DEB, 39858 (Decayed)

SL-16 DEB, 22548 (Decayed)

SL-16 DEB, 39841 (Decayed)

SL-16 DEB, 39723

SL-16 DEB, 22556 (Decayed)

SL-16 DEB, 22431 (Decayed)

SL-16 DEB, 22485 (Decayed)

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SL-16 DEB 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.
7 mins	2026-06-23 05:55:22.501Z	331.532° NNW	2026-06-23 05:58:22.501Z	275.998° WNW	43.412°	2026-06-23 06:02:22.501Z	166.817° S
7 mins	2026-06-23 20:02:22.501Z	214.18° SW	2026-06-23 20:05:22.501Z	260.888° W	40.921°	2026-06-23 20:09:22.501Z	14.358° NNE

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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 DEB, 22816 on other resources

View SL-16 DEB, 22816 on Heavens-Above

View SL-16 DEB, 22816 on Keep Track

View SL-16 DEB, 22816 on Celestrak

View SL-16 DEB, 22816 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 DEB, 22816

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-06-20T04:37:12.850Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #93 in the year 1992 (1992-12-25 UTC)

SL-16 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-16 DEB, 22816 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago