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 (1 year 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)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago

0 CZ-3B R/B
1 62486U 25002B   26029.17025473  .00154915 -79451-6  13256-2 0  9990
2 62486  28.3958 196.7235 6102015 156.6471 250.6458  3.99618824  5129

Epoch: 2026-01-29T04:05Z

TLE epoch observation values (Epoch: 2026-01-29T04:05:10.008Z)

Latitude

-0.00014°

Longitude

7.01155°

Altitude

17,540.709 km

Speed

3.093 km/s

True Right ascension

13h 06m 55s

True Declination

0° 00' 01"

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

04:19:58

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

20,637.096 km

Perigee altitude

161.726 km

Semi-major axis

16,777.548 km

Eccentricity

0.6102

Inclination

28.3958°

RAAN

196.7235°

Arg. of periapsis

156.6471°

True anomaly

203.39671°

Mean anomaly

250.6458°

Eccentric anomaly

225.64656°

Mean motion

0.99874 °/min

Orbital period

360.46 mins

BSTAR

0.0013256

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

OBJECT C, 62734

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.
239 mins	2026-01-30 07:25:01.308Z	169.643° S	2026-01-30 10:36:01.308Z	138.286° SSE	30.058°	2026-01-30 11:24:01.308Z	93.565° ESE
51 mins	2026-01-30 16:54:01.308Z	259.308° W	2026-01-30 17:39:01.308Z	199.907° SSW	36.965°	2026-01-30 17:45:01.308Z	127.845° SE

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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: 23 hours ago

TLE from 23 hours ago

TLE epoch observation values (Epoch: 2026-01-29T04:05:10.008Z)

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: 23 hours ago