SL-3 DEB, 14928
Orbit data source: Space-Track
SL-3 DEB, 14928 is space debris in SSO originally from a launch on Sun, 24 Jul 1983 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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14928 intel report (Beta)
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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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 SL-3 DEB
1 14928U 83075F 26266.89387483 .00010076 00000-0 22403-3 0 9997
2 14928 97.8261 236.2805 0018128 54.8338 305.4604 15.43713879334028Epoch: 2026-09-23T21:27Z
TLE epoch observation values (Epoch: 2026-09-23T21:27:10.785Z)
Latitude
0.00001°
Longitude
-88.2529°
Altitude
431.118 km
Speed
7.657 km/s
True Right ascension
15h 45m 07s
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
03:30:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
444.458 km
Perigee altitude
419.767 km
Semi-major axis
6,810.25 km
Eccentricity
0.00181
Inclination
97.8261°
RAAN
236.2805°
Arg. of periapsis
54.8338°
True anomaly
305.29098°
Mean anomaly
305.4604°
Eccentric anomaly
305.37571°
Mean motion
3.86188 °/min
Orbital period
93.22 mins
BSTAR
0.00022403
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Other satellites on launch #75 in the year 1983 (1983-07-24 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-3 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-24 10:28:05.804Z | 42.101° NE | 2026-09-24 10:30:05.804Z | 90.778° ESE | 29.896° | 2026-09-24 10:33:05.804Z | 160.573° S |
| 4 mins | 2026-09-24 22:29:05.804Z | 202.344° SSW | 2026-09-24 22:31:05.804Z | 275.931° WNW | 38.418° | 2026-09-24 22:33:05.804Z | 325.973° NNW |
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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