SL-8 DEB, 25028
Orbit data source: Space-Track
SL-8 DEB, 25028 is space debris in LEO originally from a launch on Wed, 16 Jun 1993 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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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25028 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: 18 hours ago
TLE from 18 hours ago
0 SL-8 DEB
1 25028U 93036D 25286.78626265 .00001646 00000-0 51636-3 0 9994
2 25028 74.0425 44.2464 0010624 306.9035 205.2784 14.41348623568388Epoch: 2025-10-13T18:52Z
TLE epoch observation values (Epoch: 2025-10-13T18:52:13.092Z)
Latitude
26.75244°
Longitude
-89.6353°
Altitude
763.855 km
Speed
7.471 km/s
True Right ascension
14h 24m 00s
True Declination
26° 36' 52"
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
07:33:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
759.238 km
Perigee altitude
744.089 km
Semi-major axis
7,129.801 km
Eccentricity
0.00106
Inclination
74.0425°
RAAN
44.2464°
Arg. of periapsis
306.9035°
True anomaly
205.22648°
Mean anomaly
205.2784°
Eccentric anomaly
205.25243°
Mean motion
3.60518 °/min
Orbital period
99.86 mins
BSTAR
0.00051636
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Other satellites on launch #36 in the year 1993 (1993-06-16 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-8 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 | 2025-10-14 18:02:23.504Z | 13.74° NNE | 2025-10-14 18:06:23.504Z | 66.64° ENE | 18.956° | 2025-10-14 18:09:23.504Z | 103.804° ESE |
| 8 mins | 2025-10-14 19:44:23.504Z | 324.206° NNW | 2025-10-14 19:48:23.504Z | 238.656° WSW | 36.57° | 2025-10-14 19:52:23.504Z | 184.331° SSW |
| 8 mins | 2025-10-15 08:36:23.504Z | 174.601° S | 2025-10-15 08:40:23.504Z | 85.448° E | 38.005° | 2025-10-15 08:44:23.504Z | 30.328° NE |
| 5 mins | 2025-10-15 10:20:23.504Z | 277.677° WNW | 2025-10-15 10:22:23.504Z | 307.006° NW | 17.929° | 2025-10-15 10:25:23.504Z | 344.296° 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 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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