CZ-4B DEB, 46472

Orbit data source: Space-Track

CZ-4B DEB, 46472 is space debris in LEO originally from a launch on Mon, 21 Sep 2020 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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https://www.satcat.com/sats-embedded/46472?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

46472, 2020-066D

Orbit

LEO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2020-09-21 (6 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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago

0 CZ-4B DEB
1 46472U 20066D   26170.96593174  .00000054  00000-0  10643-3 0  9993
2 46472  65.9117 116.6104 0029391 352.2197   7.8415 13.92352246291932

Epoch: 2026-06-19T23:10Z

TLE epoch observation values (Epoch: 2026-06-19T23:10:56.502Z)

Latitude

-0.00003°

Longitude

-139.31237°

Altitude

901.156 km

Speed

7.413 km/s

True Right ascension

07h 46m 26s

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

21:24:42

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

940.341 km

Perigee altitude

897.448 km

Semi-major axis

7,297.031 km

Eccentricity

0.00294

Inclination

65.9117°

RAAN

116.6104°

Arg. of periapsis

352.2197°

True anomaly

7.88762°

Mean anomaly

7.8415°

Eccentric anomaly

7.86454°

Mean motion

3.48196 °/min

Orbital period

103.39 mins

BSTAR

0.00010643

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Other satellites on launch #66 in the year 2020 (2020-09-21 UTC)

HAIYANG 2C, 46469

CZ-4B R/B, 46470

CZ-4B DEB, 46471

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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.
7 mins	2026-06-22 20:15:42.598Z	147.358° SSE	2026-06-22 20:19:42.598Z	99.991° ESE	19.587°	2026-06-22 20:22:42.598Z	66.297° ENE
10 mins	2026-06-22 22:00:42.598Z	227.343° WSW	2026-06-22 22:04:42.598Z	283.489° WNW	40.579°	2026-06-22 22:10:42.598Z	23.156° NE
9 mins	2026-06-23 05:17:42.598Z	357.194° N	2026-06-23 05:21:42.598Z	47.929° ENE	24.855°	2026-06-23 05:26:42.598Z	103.549° ESE
10 mins	2026-06-23 07:03:42.598Z	318.082° NNW	2026-06-23 07:08:42.598Z	232.863° WSW	39.497°	2026-06-23 07:13:42.598Z	170.502° S

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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, 46472 on other resources

View CZ-4B DEB, 46472 on Heavens-Above

View CZ-4B DEB, 46472 on Keep Track

View CZ-4B DEB, 46472 on Celestrak

View CZ-4B DEB, 46472 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, 46472

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: 2026-06-19T23:10:56.502Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #66 in the year 2020 (2020-09-21 UTC)

CZ-4B DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4B DEB, 46472 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago