SL-16 DEB, 39886
Orbit data source: Space-Track
SL-16 DEB, 39886 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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39886 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: 4 days ago
TLE from 4 days ago
0 SL-16 DEB
1 39886U 93016BL 25292.28606615 .00010072 00000-0 14370-2 0 9994
2 39886 71.0071 148.5960 0050413 258.4103 101.1390 14.76055638606700Epoch: 2025-10-19T06:51Z
TLE epoch observation values (Epoch: 2025-10-19T06:51:56.115Z)
Latitude
-0.00004°
Longitude
17.60726°
Altitude
651.281 km
Speed
7.529 km/s
True Right ascension
09h 54m 23s
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
17:40:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
675.046 km
Perigee altitude
604.288 km
Semi-major axis
7,017.804 km
Eccentricity
0.00504
Inclination
71.0071°
RAAN
148.596°
Arg. of periapsis
258.4103°
True anomaly
101.70511°
Mean anomaly
101.139°
Eccentric anomaly
101.42212°
Mean motion
3.69183 °/min
Orbital period
97.51 mins
BSTAR
0.001437
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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 | 2025-10-23 00:51:51.441Z | 341.134° N | 2025-10-23 00:56:51.441Z | 108.61° ESE | 42.409° | 2025-10-23 01:00:51.441Z | 150.641° SSE |
| 7 mins | 2025-10-23 15:05:51.441Z | 198.377° SSW | 2025-10-23 15:08:51.441Z | 142.797° SSE | 44.788° | 2025-10-23 15:12:51.441Z | 24.731° NE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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