SL-16 DEB, 22366
Orbit data source: Space-Track
SL-16 DEB, 22366 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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22366 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, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SL-16 DEB
1 22366U 92093BF 25349.64053878 .00013748 00000-0 23000-2 0 9996
2 22366 71.1061 73.5106 0067690 268.0918 241.0177 14.68398699697132Epoch: 2025-12-15T15:22Z
TLE epoch observation values (Epoch: 2025-12-15T15:22:22.550Z)
Latitude
29.74893°
Longitude
-72.83835°
Altitude
692.784 km
Speed
7.5 km/s
True Right ascension
16h 09m 10s
True Declination
29° 35' 59"
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
18:30:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
711.715 km
Perigee altitude
616.378 km
Semi-major axis
7,042.184 km
Eccentricity
0.00677
Inclination
71.1061°
RAAN
73.5106°
Arg. of periapsis
268.0918°
True anomaly
240.34195°
Mean anomaly
241.0177°
Eccentric anomaly
240.67955°
Mean motion
3.67267 °/min
Orbital period
98.02 mins
BSTAR
0.0023
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-17 06:03:27.095Z | 152.704° SSE | 2025-12-17 06:06:27.095Z | 107.412° ESE | 23.654° | 2025-12-17 06:10:27.095Z | 49.324° ENE |
| 7 mins | 2025-12-17 07:43:27.095Z | 242.935° WSW | 2025-12-17 07:46:27.095Z | 293.574° NW | 29.021° | 2025-12-17 07:50:27.095Z | 0.944° NNE |
| 7 mins | 2025-12-17 16:18:27.095Z | 351.163° N | 2025-12-17 16:21:27.095Z | 49.642° ENE | 39.407° | 2025-12-17 16:25:27.095Z | 139.503° SSE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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