SL-16 DEB, 22476
Orbit data source: Space-Track
SL-16 DEB, 22476 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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22476 intel report (Beta)
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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, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 SL-16 DEB
1 22476U 92093FR 26078.23056704 .00000743 00000-0 96187-3 0 9992
2 22476 71.5475 141.6829 0460166 107.5486 257.6408 13.27839514591333Epoch: 2026-03-19T05:32Z
TLE epoch observation values (Epoch: 2026-03-19T05:32:00.992Z)
Latitude
-0°
Longitude
-118.1042°
Altitude
1,246.457 km
Speed
7.189 km/s
True Right ascension
09h 26m 43s
True Declination
0° 00' 00"
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
16:46:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,499.429 km
Perigee altitude
806.326 km
Semi-major axis
7,531.014 km
Eccentricity
0.04602
Inclination
71.5475°
RAAN
141.6829°
Arg. of periapsis
107.5486°
True anomaly
252.55923°
Mean anomaly
257.6408°
Eccentric anomaly
255.09298°
Mean motion
3.32095 °/min
Orbital period
108.4 mins
BSTAR
0.00096187
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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 | 2026-03-24 14:29:01.684Z | 339.776° N | 2026-03-24 14:33:01.684Z | 119.635° SE | 44.73° | 2026-03-24 14:38:01.684Z | 156.938° SSE |
| 11 mins | 2026-03-25 04:28:01.684Z | 197.478° SSW | 2026-03-25 04:34:01.684Z | 153.12° SSE | 44.659° | 2026-03-25 04:39:01.684Z | 24.379° NE |
| 4 mins | 2026-03-25 06:24:01.684Z | 289.916° WNW | 2026-03-25 06:26:01.684Z | 312.527° NW | 14.639° | 2026-03-25 06:28:01.684Z | 334.933° NNW |
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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