SL-16 DEB, 22617

Orbit data source: Space-Track

SL-16 DEB, 22617 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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Iframe URL

https://www.satcat.com/sats-embedded/22617?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

22617, 1993-016AB

Orbit

LEO

Last TLE update

15 hours ago

Origin

Russian Strategic Rocket Forces (CIS)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1993-03-26 (32 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

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 15 hours ago

0 SL-16 DEB
1 22617U 93016AB  25199.34869808  .00000336  00000-0  27815-3 0  9997
2 22617  70.9991  58.1701 0134534 278.1192 258.9945 13.91929834634056

Epoch: 2025-07-18T08:22Z

TLE epoch observation values (Epoch: 2025-07-18T08:22:07.514Z)

Latitude

4.07431°

Longitude

174.8392°

Altitude

943.833 km

Speed

7.37 km/s

True Right ascension

15h 47m 05s

True Declination

4° 03' 02"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

20.84057°

Longitude

2.48607°

Altitude

947.873 km

Speed

7.368 km/s

Apparent Right ascension

02h 31m 12s

Apparent Declination

-8° 27' 37"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

11:56:02

Azimuth

301.645° NW

Elevation

-43.293°

Doppler factor

Orbital elements

Apogee altitude

1,018.005 km

Perigee altitude

821.64 km

Semi-major axis

7,297.96 km

Eccentricity

0.01345

Inclination

70.9991°

RAAN

58.1701°

Arg. of periapsis

278.1192°

True anomaly

257.48622°

Mean anomaly

258.9945°

Eccentric anomaly

258.23986°

Mean motion

3.4813 °/min

Orbital period

103.41 mins

BSTAR

0.00027815

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

SL-16 DEB, 22661 (Decayed)

SL-16 DEB, 23304 (Decayed)

SL-16 DEB, 26968

SL-16 DEB *, 29096 (Decayed)

SL-16 DEB, 29097

SL-16 DEB, 29098

SL-16 DEB, 29099 (Decayed)

SL-16 DEB, 29100

SL-16 DEB Visibility forecast

Observer location: undefined°, undefined°

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	2025-07-19 01:20:29.117Z	348.694° N	2025-07-19 01:25:29.117Z	76.277° E	40.3°	2025-07-19 01:30:29.117Z	140.046° SSE
7 mins	2025-07-19 03:07:29.117Z	295.707° NW	2025-07-19 03:10:29.117Z	260.525° W	21.032°	2025-07-19 03:14:29.117Z	216.873° SW
8 mins	2025-07-19 14:41:29.117Z	139.356° SSE	2025-07-19 14:44:29.117Z	103.166° ESE	22.274°	2025-07-19 14:49:29.117Z	49.839° ENE
10 mins	2025-07-19 16:25:29.117Z	225.709° WSW	2025-07-19 16:30:29.117Z	311.661° NW	38.624°	2025-07-19 16:35:29.117Z	12.231° NNE

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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Check out SL-16 DEB, 22617 on other resources

View SL-16 DEB, 22617 on Heavens-Above

View SL-16 DEB, 22617 on Keep Track

View SL-16 DEB, 22617 on Celestrak

View SL-16 DEB, 22617 on Gunter's Space Page

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