CZ-4B DEB, 48625

Orbit data source: Space-Track

CZ-4B DEB, 48625 is space debris in LEO originally from a launch on Wed, 19 May 2021 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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/48625?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

48625, 2021-043E

Orbit

LEO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2021-05-19 (5 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

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

TLE from 6 days ago

0 CZ-4B DEB
1 48625U 21043E   26167.52535468  .00001238  00000-0  92924-3 0  9998
2 48625  66.1670 267.3572 0049972 266.9485  92.5873 13.97421099258156

Epoch: 2026-06-16T12:36Z

TLE epoch observation values (Epoch: 2026-06-16T12:36:30.644Z)

Latitude

-0.00002°

Longitude

173.43337°

Altitude

906.597 km

Speed

7.398 km/s

True Right ascension

17h 49m 25s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

00:27:00

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

937.577 km

Perigee altitude

864.824 km

Semi-major axis

7,279.338 km

Eccentricity

0.005

Inclination

66.167°

RAAN

267.3572°

Arg. of periapsis

266.9485°

True anomaly

93.15918°

Mean anomaly

92.5873°

Eccentric anomaly

92.87326°

Mean motion

3.49466 °/min

Orbital period

103.01 mins

BSTAR

0.00092924

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Other satellites on launch #43 in the year 2021 (2021-05-19 UTC)

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CZ-4B DEB 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.
10 mins	2026-06-22 15:08:30.285Z	348.738° N	2026-06-22 15:13:30.285Z	50.538° ENE	28.671°	2026-06-22 15:18:30.285Z	110.987° ESE
9 mins	2026-06-22 16:55:30.285Z	310.24° NW	2026-06-22 16:59:30.285Z	249.679° W	34.593°	2026-06-22 17:04:30.285Z	180.902° SSW
9 mins	2026-06-23 06:11:30.285Z	172.149° S	2026-06-23 06:15:30.285Z	115.169° SE	32.932°	2026-06-23 06:20:30.285Z	47.404° ENE
9 mins	2026-06-23 07:57:30.285Z	251.546° W	2026-06-23 08:01:30.285Z	305.385° NW	30.099°	2026-06-23 08:06:30.285Z	11.191° NNE

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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-4B DEB, 48625 on other resources

View CZ-4B DEB, 48625 on Heavens-Above

View CZ-4B DEB, 48625 on Keep Track

View CZ-4B DEB, 48625 on Celestrak

View CZ-4B DEB, 48625 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-4B DEB, 48625

Orbit data source: Space-Track

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

TLE from 6 days ago

TLE epoch observation values (Epoch: 2026-06-16T12:36:30.644Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #43 in the year 2021 (2021-05-19 UTC)

CZ-4B DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4B DEB, 48625 on other resources

Documentation

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