CZ-3B R/B, 62805
Orbit data source: Space-Track
CZ-3B R/B, 62805 is space debris in HEO 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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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
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: 9 hours ago
TLE from 9 hours ago
0 CZ-3B R/B
1 62805U 25017B 25292.86677072 .00361812 49708-7 69527-3 0 9997
2 62805 28.0737 214.0207 6529276 46.7490 351.7962 3.37697821 7975Epoch: 2025-10-19T20:48Z
TLE epoch observation values (Epoch: 2025-10-19T20:48:08.990Z)
Latitude
0.00014°
Longitude
-126.56804°
Altitude
1,059.223 km
Speed
9.271 km/s
True Right ascension
14h 16m 11s
True Declination
0° 00' 01"
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
01:02:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
24,647.49 km
Perigee altitude
136.449 km
Semi-major axis
18,770.107 km
Eccentricity
0.65293
Inclination
28.0737°
RAAN
214.0207°
Arg. of periapsis
46.749°
True anomaly
312.97364°
Mean anomaly
351.7962°
Eccentric anomaly
337.44964°
Mean motion
0.844 °/min
Orbital period
426.54 mins
BSTAR
0.00069527
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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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 53 mins | 2025-10-20 06:06:54.065Z | 135.278° SSE | 2025-10-20 06:06:54.065Z | 135.278° SSE | 13.583° | 2025-10-20 06:59:54.065Z | 138.635° SSE |
| 17 mins | 2025-10-21 01:29:54.065Z | 194.279° SSW | 2025-10-21 01:31:54.065Z | 158.202° S | 27.7° | 2025-10-21 01:46:54.065Z | 106.296° ESE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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