SL-16 DEB, 22393
Orbit data source: Space-Track
SL-16 DEB, 22393 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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22393 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 SL-16 DEB
1 22393U 92093CJ 25317.41595580 .00004784 00000-0 25979-2 0 9994
2 22393 71.1224 304.1874 0118644 338.3760 173.0119 14.09276599677700Epoch: 2025-11-13T09:58Z
TLE epoch observation values (Epoch: 2025-11-13T09:58:58.581Z)
Latitude
26.83758°
Longitude
-88.24122°
Altitude
949.895 km
Speed
7.336 km/s
True Right ascension
07h 37m 06s
True Declination
26° 42' 11"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
17:58:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
945.64 km
Perigee altitude
773.893 km
Semi-major axis
7,237.903 km
Eccentricity
0.01186
Inclination
71.1224°
RAAN
304.1874°
Arg. of periapsis
338.376°
True anomaly
173.17491°
Mean anomaly
173.0119°
Eccentric anomaly
173.09364°
Mean motion
3.52471 °/min
Orbital period
102.14 mins
BSTAR
0.0025979
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Other satellites on launch #93 in the year 1992 (1992-12-25 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-14 00:44:18.952Z | 204.312° SW | 2025-11-14 00:47:18.952Z | 221.6° SW | 44.282° | 2025-11-14 00:53:18.952Z | 22.14° NNE |
| 10 mins | 2025-11-14 09:40:18.952Z | 355.281° N | 2025-11-14 09:44:18.952Z | 49.063° ENE | 34.312° | 2025-11-14 09:50:18.952Z | 131.08° SE |
| 8 mins | 2025-11-14 11:25:18.952Z | 306.262° NW | 2025-11-14 11:29:18.952Z | 252.785° W | 26.124° | 2025-11-14 11:33:18.952Z | 205.257° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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