SL-16 DEB, 22350

Orbit data source: Space-Track

SL-16 DEB, 22350 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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<iframe src="https://www.satcat.com/sats-embedded/22350?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/22350?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

Identifier

22350, 1992-093AP

Orbit

LEO

Last TLE update

6 hours ago

Origin

Russian Strategic Rocket Forces (CIS)

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

Radar Cross Section

0.380 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 6 hours ago

0 SL-16 DEB
1 22350U 92093AP  25186.97795242 -.00000022  00000-0  15433-4 0  9997
2 22350  70.9103  65.4460 0070689 235.0696 224.1475 14.06155862667259

Epoch: 2025-07-05T23:28Z

TLE epoch observation values (Epoch: 2025-07-05T23:28:15.089Z)

Latitude

69.20187°

Longitude

-95.83609°

Altitude

920.934 km

Speed

7.379 km/s

True Right ascension

12h 01m 44s

True Declination

69° 05' 24"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-23.2975°

Longitude

-22.78719°

Altitude

836.352 km

Speed

7.457 km/s

Apparent Right ascension

16h 28m 39s

Apparent Declination

-75° 49' 29"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

17:02:55

Azimuth

182.323° SSW

Elevation

-25.874°

Doppler factor

Orbital elements

Apogee altitude

921.738 km

Perigee altitude

819.259 km

Semi-major axis

7,248.635 km

Eccentricity

0.00707

Inclination

70.9103°

RAAN

65.446°

Arg. of periapsis

235.0696°

True anomaly

Unknown

Mean anomaly

224.1475°

Eccentric anomaly

Unknown

Mean motion

3.51689 °/min

Orbital period

102.36 mins

BSTAR

0.000015433

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

SL-16 DEB, 22345 (Decayed)

SL-16 DEB, 22346 (Decayed)

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.
9 mins	2025-07-06 16:10:38.215Z	154.64° SSE	2025-07-06 16:15:38.215Z	97.858° ESE	23.396°	2025-07-06 16:19:38.215Z	51.859° ENE
10 mins	2025-07-06 17:55:38.215Z	231.074° WSW	2025-07-06 17:59:38.215Z	292.769° NW	36.612°	2025-07-06 18:05:38.215Z	12.685° NNE
4 mins	2025-07-07 01:10:38.215Z	26.849° NE	2025-07-07 01:12:38.215Z	48.672° ENE	13.544°	2025-07-07 01:14:38.215Z	70.136° E
10 mins	2025-07-07 02:53:38.215Z	339.672° N	2025-07-07 02:58:38.215Z	123.97° SE	43.915°	2025-07-07 03:03:38.215Z	154.412° SSE

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Check out SL-16 DEB, 22350 on other resources

View SL-16 DEB, 22350 on Heavens-Above

View SL-16 DEB, 22350 on Keep Track

View SL-16 DEB, 22350 on Celestrak

View SL-16 DEB, 22350 on Gunter's Space Page

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