SL-14 R/B, 17296
Orbit data source: Space-Track
SL-14 R/B, 17296 is space debris in LEO originally from a launch on Wed, 14 Jan 1987 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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17296 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Yuzhnoe
Mission
Spacecraft
Bus & Motor
S5M, Unknown motor
Mass
1,600 kg wet, 1,600 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.4 m
Radar Cross Section
7.351 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 SL-14 R/B
1 17296U 87003B 26122.03571079 .00000424 00000-0 46045-4 0 9991
2 17296 82.5302 230.9590 0017216 331.3826 28.6444 14.85677702102624Epoch: 2026-05-02T00:51Z
TLE epoch observation values (Epoch: 2026-05-02T00:51:25.412Z)
Latitude
0.00003°
Longitude
-1.85627°
Altitude
603.943 km
Speed
7.563 km/s
True Right ascension
15h 23m 50s
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
19:55:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
620.502 km
Perigee altitude
596.446 km
Semi-major axis
6,986.611 km
Eccentricity
0.00172
Inclination
82.5302°
RAAN
230.959°
Arg. of periapsis
331.3826°
True anomaly
28.73915°
Mean anomaly
28.6444°
Eccentric anomaly
28.69176°
Mean motion
3.71658 °/min
Orbital period
96.86 mins
BSTAR
0.000046045
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Other satellites on launch #3 in the year 1987 (1987-01-14 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-14 R/B 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-02 19:12:03.635Z | 351.077° N | 2026-05-02 19:16:03.635Z | 210.327° SW | 44.671° | 2026-05-02 19:20:03.635Z | 175.904° S |
| 7 mins | 2026-05-03 07:42:03.635Z | 169.058° S | 2026-05-03 07:45:03.635Z | 80.973° E | 40.769° | 2026-05-03 07:49:03.635Z | 15.228° NNE |
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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