SL-8 DEB, 22025

Orbit data source: Space-Track

SL-8 DEB, 22025 is space debris in LEO originally from a launch on Tue, 12 Feb 1991 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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https://www.satcat.com/sats-embedded/22025?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

22025, 1991-009CJ

Orbit

LEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1991-02-12 (35 years ago)

Launch vehicle

Unknown

Launch site

Plesetsk Missile And Space Complex (PKMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 SL-8 DEB
1 22025U 91009CJ  26070.44045682  .00000106  00000-0  97497-3 0  9994
2 22025  73.9380 228.1614 0144653 148.1490 243.6691 12.31710543573314

Epoch: 2026-03-11T10:34Z

TLE epoch observation values (Epoch: 2026-03-11T10:34:15.469Z)

Latitude

29.09166°

Longitude

-90.33427°

Altitude

1,597.191 km

Speed

7.05 km/s

True Right ascension

15h 49m 20s

True Declination

28° 57' 40"

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

15:22:06

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,654.338 km

Perigee altitude

1,425.267 km

Semi-major axis

7,917.94 km

Eccentricity

0.01447

Inclination

73.938°

RAAN

228.1614°

Arg. of periapsis

148.149°

True anomaly

242.19547°

Mean anomaly

243.6691°

Eccentric anomaly

242.93109°

Mean motion

3.08053 °/min

Orbital period

116.86 mins

BSTAR

0.00097497

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Other satellites on launch #9 in the year 1991 (1991-02-12 UTC)

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SL-8 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.
17 mins	2026-03-12 11:50:08.394Z	205.081° SW	2026-03-12 11:59:08.394Z	314.653° NW	43.931°	2026-03-12 12:07:08.394Z	15.992° NNE
10 mins	2026-03-12 13:55:08.394Z	279.716° WNW	2026-03-12 14:00:08.394Z	316.32° NNW	17.178°	2026-03-12 14:05:08.394Z	351.749° N
12 mins	2026-03-12 20:09:08.394Z	7.422° NNE	2026-03-12 20:14:08.394Z	51.877° ENE	25.373°	2026-03-12 20:21:08.394Z	110.658° ESE
15 mins	2026-03-12 22:07:08.394Z	333.62° NNW	2026-03-12 22:14:08.394Z	265.064° W	42.043°	2026-03-12 22:22:08.394Z	178.233° S
6 mins	2026-03-13 09:21:08.394Z	105.284° ESE	2026-03-13 09:23:08.394Z	91.484° ESE	14.008°	2026-03-13 09:27:08.394Z	63.816° ENE

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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-8 DEB, 22025 on other resources

View SL-8 DEB, 22025 on Heavens-Above

View SL-8 DEB, 22025 on Keep Track

View SL-8 DEB, 22025 on Celestrak

View SL-8 DEB, 22025 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-8 DEB, 22025

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-03-11T10:34:15.469Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #9 in the year 1991 (1991-02-12 UTC)

SL-8 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-8 DEB, 22025 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago