CZ-2C R/B, 61620 (Decayed)
Orbit data source: Space-Track
CZ-2C R/B, 61620 was space debris in LEO originally from a launch on Wed, 23 Oct 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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61620 intel report (Beta)
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Edit Public Description
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: 10 months ago
TLE from 10 months ago
0 CZ-2C R/B
1 61620U 24190D 24325.87196646 .05332485 15058-5 50849-3 0 9997
2 61620 34.9970 184.6356 0040246 310.7409 119.6211 16.34319024 4516Epoch: 2024-11-20T20:55Z
TLE epoch observation values (Epoch: 2024-11-20T20:55:37.902Z)
Latitude
32.9322°
Longitude
-122.73039°
Altitude
194.193 km
Speed
7.788 km/s
True Right ascension
16h 46m 09s
True Declination
32° 45' 43"
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
14:08:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
210.777 km
Perigee altitude
157.954 km
Semi-major axis
6,562.502 km
Eccentricity
0.00402
Inclination
34.997°
RAAN
184.6356°
Arg. of periapsis
310.7409°
True anomaly
120.02102°
Mean anomaly
119.6211°
Eccentric anomaly
119.82116°
Mean motion
4.08262 °/min
Orbital period
88.18 mins
BSTAR
0.00050849
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Other satellites on launch #190 in the year 2024 (2024-10-23 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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