CZ-2C R/B, 55691 (Decayed)
Orbit data source: Space-Track
CZ-2C R/B, 55691 was space debris in LEO originally from a launch on Fri, 24 Feb 2023 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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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55691 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
~3,800 kg wet, ~3,800 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 3.7 m
Radar Cross Section
23.715 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 CZ-2C R/B
1 55691U 23025B 26042.90185454 .13281244 26567-5 14546-3 0 9997
2 55691 97.5194 166.9544 0010163 282.3890 227.2631 16.50138957166664Epoch: 2026-02-11T21:38Z
TLE epoch observation values (Epoch: 2026-02-11T21:38:40.232Z)
Latitude
30.20226°
Longitude
-115.29358°
Altitude
147.518 km
Speed
7.818 km/s
True Right ascension
23h 25m 20s
True Declination
30° 02' 20"
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
21:32:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
142.39 km
Perigee altitude
129.149 km
Semi-major axis
6,513.907 km
Eccentricity
0.00102
Inclination
97.5194°
RAAN
166.9544°
Arg. of periapsis
282.389°
True anomaly
227.17764°
Mean anomaly
227.2631°
Eccentric anomaly
227.22036°
Mean motion
4.12839 °/min
Orbital period
87.2 mins
BSTAR
0.00014546
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Other satellites on launch #25 in the year 2023 (2023-02-24 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.CZ-2C 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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