CZ-3B R/B, 62805
Orbit data source: Space-Track
CZ-3B R/B, 62805 is space debris in LEO originally from a launch on Thu, 23 Jan 2025 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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62805 intel report (Beta)
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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
Cyl + 1 Nozzle, 4.5 m
Radar Cross Section
32.704 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 CZ-3B R/B
1 62805U 25017B 26090.97165823 .19529838 -11929-4 90435-3 0 9990
2 62805 28.0022 323.5473 1502001 97.1238 280.1868 13.00780187 18112Epoch: 2026-03-31T23:19Z
TLE epoch observation values (Epoch: 2026-03-31T23:19:11.271Z)
Latitude
-0°
Longitude
144.40914°
Altitude
1,225.676 km
Speed
7.259 km/s
True Right ascension
21h 34m 11s
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
19:54:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,410.74 km
Perigee altitude
115.331 km
Semi-major axis
7,641.172 km
Eccentricity
0.1502
Inclination
28.0022°
RAAN
323.5473°
Arg. of periapsis
97.1238°
True anomaly
262.93102°
Mean anomaly
280.1868°
Eccentric anomaly
271.58426°
Mean motion
3.2494 °/min
Orbital period
110.79 mins
BSTAR
0.00090435
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Other satellites on launch #17 in the year 2025 (2025-01-23 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-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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| CZ-3B R/B is likely not visible in the next few days. |
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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