SL-4 R/B, 62217 (Decayed)
Orbit data source: Space-Track
SL-4 R/B, 62217 was space debris in LEO originally from a launch on Wed, 04 Dec 2024 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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62217 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
TsSKB-Progress
Mission
Decayed spacecraft
Bus & Motor
BLOK-I, Unknown motor
Mass
~2,350 kg wet, 2,350 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 3.5 m
Radar Cross Section
17.919 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 SL-4 R/B
1 62217U 24230B 25127.53339538 .11780966 65361-5 10067-3 0 9996
2 62217 67.0785 218.1437 0036280 286.1851 143.1106 16.48493623 23725Epoch: 2025-05-07T12:48Z
TLE epoch observation values (Epoch: 2025-05-07T12:48:05.360Z)
Latitude
59.77811°
Longitude
-153.29768°
Altitude
171.581 km
Speed
7.798 km/s
True Right ascension
17h 37m 21s
True Declination
59° 36' 53"
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
02:58:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
165.123 km
Perigee altitude
117.816 km
Semi-major axis
6,519.607 km
Eccentricity
0.00363
Inclination
67.0785°
RAAN
218.1437°
Arg. of periapsis
286.1851°
True anomaly
143.35925°
Mean anomaly
143.1106°
Eccentric anomaly
143.23502°
Mean motion
4.12298 °/min
Orbital period
87.32 mins
BSTAR
0.00010067
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Other satellites on launch #230 in the year 2024 (2024-12-04 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-4 R/B Visibility
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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. |
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| This satellite is decayed. |
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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