CZ-3B R/B, 62486

Orbit data source: Space-Track

CZ-3B R/B, 62486 is space debris in HEO originally from a launch on Mon, 06 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/62486?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

62486, 2025-002B

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)

2025-01-06 (11 months ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 1 Nozzle, 3.3 m

Radar Cross Section

32.704 m², Large (>1 m²)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 CZ-3B R/B
1 62486U 25002B   25346.33527534  .00176928  37987-6  88490-3 0  9992
2 62486  28.3638 232.1525 6200276  98.9610 331.4200  3.85448582  3243

Epoch: 2025-12-12T08:02Z

TLE epoch observation values (Epoch: 2025-12-12T08:02:47.789Z)

Latitude

0.00003°

Longitude

30.21219°

Altitude

5,323.401 km

Speed

6.703 km/s

True Right ascension

15h 28m 45s

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

11:03:52

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

21,463.982 km

Perigee altitude

152.145 km

Semi-major axis

17,186.2 km

Eccentricity

0.62003

Inclination

28.3638°

RAAN

232.1525°

Arg. of periapsis

98.961°

True anomaly

261.07473°

Mean anomaly

331.42°

Eccentric anomaly

300.95471°

Mean motion

0.96333 °/min

Orbital period

373.71 mins

BSTAR

0.0008849

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Other satellites on launch #2 in the year 2025 (2025-01-06 UTC)

SJ-25, 62485

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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.
112 mins	2025-12-13 13:18:32.799Z	188.731° SSW	2025-12-13 14:48:32.799Z	166.13° S	15.332°	2025-12-13 15:10:32.799Z	138.22° 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, 62486 on other resources

View CZ-3B R/B, 62486 on Heavens-Above

View CZ-3B R/B, 62486 on Keep Track

View CZ-3B R/B, 62486 on Celestrak

View CZ-3B R/B, 62486 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, 62486

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2025-12-12T08:02:47.789Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #2 in the year 2025 (2025-01-06 UTC)

CZ-3B R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-3B R/B, 62486 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago