SL-16 DEB, 26968
Orbit data source: Space-Track
SL-16 DEB, 26968 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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26968 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: 13 hours ago
TLE from 13 hours ago
0 SL-16 DEB
1 26968U 93016AJ 25309.29575769 .00003186 00000-0 97589-3 0 9998
2 26968 70.9977 35.4343 0009744 242.4563 174.3241 14.42467066697008Epoch: 2025-11-05T07:05Z
TLE epoch observation values (Epoch: 2025-11-05T07:05:53.464Z)
Latitude
52.39993°
Longitude
-89.39895°
Altitude
765.247 km
Speed
7.473 km/s
True Right ascension
04h 07m 22s
True Declination
52° 14' 01"
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
16:18:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
755.201 km
Perigee altitude
741.313 km
Semi-major axis
7,126.394 km
Eccentricity
0.00097
Inclination
70.9977°
RAAN
35.4343°
Arg. of periapsis
242.4563°
True anomaly
174.33513°
Mean anomaly
174.3241°
Eccentric anomaly
174.32962°
Mean motion
3.60777 °/min
Orbital period
99.78 mins
BSTAR
0.00097589
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-06 06:15:45.192Z | 151.299° SSE | 2025-11-06 06:18:45.192Z | 109.077° ESE | 23.582° | 2025-11-06 06:22:45.192Z | 51.771° ENE |
| 7 mins | 2025-11-06 07:57:45.192Z | 242.766° WSW | 2025-11-06 08:00:45.192Z | 295.511° NW | 31.037° | 2025-11-06 08:04:45.192Z | 2.057° NNE |
| 8 mins | 2025-11-06 16:41:45.192Z | 345.642° N | 2025-11-06 16:44:45.192Z | 34.007° NE | 42.37° | 2025-11-06 16:49:45.192Z | 148.384° 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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