SL-16 DEB, 39717
Orbit data source: Space-Track
SL-16 DEB, 39717 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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39717 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 SL-16 DEB
1 39717U 92093KH 26035.39077504 .00000528 00000-0 35527-3 0 9991
2 39717 70.6877 50.2894 0096247 137.8860 222.9703 14.03172511603833Epoch: 2026-02-04T09:22Z
TLE epoch observation values (Epoch: 2026-02-04T09:22:42.963Z)
Latitude
-0.00004°
Longitude
135.05234°
Altitude
936.649 km
Speed
7.358 km/s
True Right ascension
03h 21m 09s
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
05:23:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
950.662 km
Perigee altitude
810.932 km
Semi-major axis
7,258.934 km
Eccentricity
0.00962
Inclination
70.6877°
RAAN
50.2894°
Arg. of periapsis
137.886°
True anomaly
222.22512°
Mean anomaly
222.9703°
Eccentric anomaly
222.59705°
Mean motion
3.50941 °/min
Orbital period
102.58 mins
BSTAR
0.00035527
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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 | 2026-02-12 09:32:45.080Z | 357.885° N | 2026-02-12 09:36:45.080Z | 47.614° ENE | 26.224° | 2026-02-12 09:41:45.080Z | 116.522° SE |
| 8 mins | 2026-02-12 11:18:45.080Z | 310.245° NW | 2026-02-12 11:21:45.080Z | 264.94° W | 29.933° | 2026-02-12 11:26:45.080Z | 191.782° SSW |
| 9 mins | 2026-02-13 00:31:45.080Z | 194.108° SSW | 2026-02-13 00:35:45.080Z | 125.499° SE | 44.181° | 2026-02-13 00:40:45.080Z | 27.313° NE |
| 6 mins | 2026-02-13 02:18:45.080Z | 277.999° WNW | 2026-02-13 02:21:45.080Z | 313.41° NW | 16.489° | 2026-02-13 02:24:45.080Z | 347.085° N |
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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