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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Iframe URL

https://www.satcat.com/sats-embedded/62805?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

62805, 2025-017B

Orbit

HEO

Country

CN / PRC

Related business

China Aerospace Science and Technology Corporation (CASC) (CN)

Manufacturer

CALT

Mission

Spacecraft

Bus & Motor

CZ-3A STAGE 3, Unknown motor

Mass

~2,800 kg wet, ~2,800 kg dry

Launch date (UTC)

2025-01-23 (8 months ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 1 Nozzle, 6.2 m

Radar Cross Section

32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 months ago

TLE from 6 months ago

0 CZ-3B R/B
1 62805U 25017B   25081.74146979  .00331763 -15108-6  18890-2 0  9992
2 62805  28.3805 329.5012 7064469 218.0597  60.6590  2.62104442  1416

Epoch: 2025-03-22T17:47Z

TLE epoch observation values (Epoch: 2025-03-22T17:47:42.989Z)

Latitude

0.00008°

Longitude

-117.89542°

Altitude

18,714.268 km

Speed

3.719 km/s

True Right ascension

21h 58m 03s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

21:51:40

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

31,546.16 km

Perigee altitude

145.825 km

Semi-major axis

22,224.129 km

Eccentricity

0.70645

Inclination

28.3805°

RAAN

329.5012°

Arg. of periapsis

218.0597°

True anomaly

141.91248°

Mean anomaly

60.659°

Eccentric anomaly

100.46247°

Mean motion

0.6551 °/min

Orbital period

549.54 mins

BSTAR

0.001889

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Other satellites on launch #17 in the year 2025 (2025-01-23 UTC)

TJS-14, 62804

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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.
284 mins	2025-09-16 05:59:30.239Z	262.197° W	2025-09-16 06:34:30.239Z	188.548° SSW	42.45°	2025-09-16 10:43:30.239Z	150.006° SSE
30 mins	2025-09-17 00:45:30.239Z	162.352° S	2025-09-17 00:51:30.239Z	121.24° SE	20.973°	2025-09-17 01:15:30.239Z	83.804° E

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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Check out CZ-3B R/B, 62805 on other resources

View CZ-3B R/B, 62805 on Heavens-Above

View CZ-3B R/B, 62805 on Keep Track

View CZ-3B R/B, 62805 on Celestrak

View CZ-3B R/B, 62805 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

CZ-3B R/B, 62805

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 6 months ago

TLE from 6 months ago

TLE epoch observation values (Epoch: 2025-03-22T17:47:42.989Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #17 in the year 2025 (2025-01-23 UTC)

CZ-3B R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-3B R/B, 62805 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 6 months ago