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 (10 months ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 1 Nozzle, 4.5 m

Radar Cross Section

32.704 m², Large (>1 m²)

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Last TLE update: 2 days ago

TLE from 2 days ago

0 CZ-3B R/B
1 62805U 25017B   25337.94420837  .00474642 -29807-6  42872-3 0  9999
2 62805  28.0576 182.9416 5996075  97.4321 330.2659  4.19058462  9634

Epoch: 2025-12-03T22:39Z

TLE epoch observation values (Epoch: 2025-12-03T22:39:39.603Z)

Latitude

-0.00003°

Longitude

130.06194°

Altitude

4,885.611 km

Speed

6.801 km/s

True Right ascension

12h 11m 56s

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

14:37:04

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

19,623.072 km

Perigee altitude

130.14 km

Semi-major axis

16,254.743 km

Eccentricity

0.59961

Inclination

28.0576°

RAAN

182.9416°

Arg. of periapsis

97.4321°

True anomaly

262.66799°

Mean anomaly

330.2659°

Eccentric anomaly

300.73704°

Mean motion

1.0473 °/min

Orbital period

343.74 mins

BSTAR

0.00042872

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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.
61 mins	2025-12-06 12:35:37.169Z	200.828° SSW	2025-12-06 13:23:37.169Z	170.952° S	17.459°	2025-12-06 13:36:37.169Z	136.685° SSE

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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: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2025-12-03T22:39:39.603Z)

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: 2 days ago