SL-16 DEB, 22616
Orbit data source: Space-Track
SL-16 DEB, 22616 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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22616 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, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 SL-16 DEB
1 22616U 93016AA 25312.50096589 .00000111 00000-0 14364-3 0 9995
2 22616 70.9962 331.3297 0185047 131.5102 20.4660 13.73962727634770Epoch: 2025-11-08T12:01Z
TLE epoch observation values (Epoch: 2025-11-08T12:01:23.452Z)
Latitude
25.71034°
Longitude
-86.44192°
Altitude
860.585 km
Speed
7.489 km/s
True Right ascension
09h 27m 20s
True Declination
25° 34' 41"
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
20:37:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,119.565 km
Perigee altitude
847.121 km
Semi-major axis
7,361.48 km
Eccentricity
0.0185
Inclination
70.9962°
RAAN
331.3297°
Arg. of periapsis
131.5102°
True anomaly
21.22382°
Mean anomaly
20.466°
Eccentric anomaly
20.84325°
Mean motion
3.43633 °/min
Orbital period
104.76 mins
BSTAR
0.00014364
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Other satellites on launch #16 in the year 1993 (1993-03-26 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-09 01:23:06.113Z | 142.916° SSE | 2025-11-09 01:27:06.113Z | 104.737° ESE | 18.438° | 2025-11-09 01:31:06.113Z | 61.253° ENE |
| 11 mins | 2025-11-09 03:09:06.113Z | 216.286° SW | 2025-11-09 03:14:06.113Z | 290.824° WNW | 42.072° | 2025-11-09 03:20:06.113Z | 17.018° NNE |
| 10 mins | 2025-11-09 12:20:06.113Z | 341.927° N | 2025-11-09 12:24:06.113Z | 28.157° NE | 43.337° | 2025-11-09 12:30:06.113Z | 151.561° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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