CZ-3B R/B, 61188 (Decayed)
Orbit data source: Space-Track
CZ-3B R/B, 61188 was space debris in LEO originally from a launch on Thu, 19 Sep 2024 UTC launched from the Xichang Space Center, China (XSC). 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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61188 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 6.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 days ago
TLE from 6 days ago
0 CZ-3B R/B
1 61188U 24168D 25261.96809037 .44772238 11702-4 11910-2 0 9999
2 61188 54.5391 355.2244 0850909 357.4567 2.2221 14.54629055 21740Epoch: 2025-09-18T23:14Z
TLE epoch observation values (Epoch: 2025-09-18T23:14:03.007Z)
Latitude
-0.00003°
Longitude
8.58977°
Altitude
108.95 km
Speed
8.168 km/s
True Right ascension
23h 40m 53s
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
08:48:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,313.792 km
Perigee altitude
107.417 km
Semi-major axis
7,088.741 km
Eccentricity
0.08509
Inclination
54.5391°
RAAN
355.2244°
Arg. of periapsis
357.4567°
True anomaly
2.64488°
Mean anomaly
2.2221°
Eccentric anomaly
2.4287°
Mean motion
3.63655 °/min
Orbital period
98.99 mins
BSTAR
0.001191
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Other satellites on launch #168 in the year 2024 (2024-09-19 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-3B 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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