SL-16 DEB, 29100
Orbit data source: Space-Track
SL-16 DEB, 29100 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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29100 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: 11 hours ago
TLE from 11 hours ago
0 SL-16 DEB
1 29100U 93016AP 25294.43009975 .00001386 00000-0 76836-3 0 9991
2 29100 70.7317 218.8149 0069868 66.5385 294.3059 14.11833450197719Epoch: 2025-10-21T10:19Z
TLE epoch observation values (Epoch: 2025-10-21T10:19:20.618Z)
Latitude
0.00007°
Longitude
33.86084°
Altitude
834.979 km
Speed
7.446 km/s
True Right ascension
14h 35m 15s
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
16:18:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
901.568 km
Perigee altitude
800.55 km
Semi-major axis
7,229.196 km
Eccentricity
0.00699
Inclination
70.7317°
RAAN
218.8149°
Arg. of periapsis
66.5385°
True anomaly
293.57363°
Mean anomaly
294.3059°
Eccentric anomaly
293.94002°
Mean motion
3.53109 °/min
Orbital period
101.95 mins
BSTAR
0.00076836
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-22 05:35:06.091Z | 354.575° N | 2025-10-22 05:39:06.091Z | 60.025° ENE | 34.903° | 2025-10-22 05:44:06.091Z | 131.69° SE |
| 7 mins | 2025-10-22 07:20:06.091Z | 299.491° NW | 2025-10-22 07:23:06.091Z | 258.455° W | 22.519° | 2025-10-22 07:27:06.091Z | 208.607° SW |
| 9 mins | 2025-10-22 20:28:06.091Z | 207.802° SW | 2025-10-22 20:32:06.091Z | 319.759° NNW | 44.464° | 2025-10-22 20:37:06.091Z | 21.166° NNE |
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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