CZ-4C R/B, 57655

Orbit data source: Space-Track

CZ-4C R/B, 57655 is space debris in SSO originally from a launch on Sun, 20 Aug 2023 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/57655?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

57655, 2023-123B

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

CZ-4 STAGE 3, Unknown motor

Mass

~1,000 kg wet, ~1,000 kg dry

Launch date (UTC)

2023-08-20 (2 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 1.4 m

Radar Cross Section

7.676 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago

0 CZ-4C R/B
1 57655U 23123B   25344.67693534  .00023316  00000-0  66816-3 0  9995
2 57655  97.9559 314.3429 0065607  22.7555 337.6570 15.33738425128126

Epoch: 2025-12-10T16:14Z

TLE epoch observation values (Epoch: 2025-12-10T16:14:47.213Z)

Latitude

-0.00003°

Longitude

-8.99765°

Altitude

426.273 km

Speed

7.679 km/s

True Right ascension

20h 57m 22s

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

01:54:43

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

506.516 km

Perigee altitude

416.768 km

Semi-major axis

6,839.779 km

Eccentricity

0.00656

Inclination

97.9559°

RAAN

314.3429°

Arg. of periapsis

22.7555°

True anomaly

337.36902°

Mean anomaly

337.657°

Eccentric anomaly

337.51323°

Mean motion

3.8369 °/min

Orbital period

93.83 mins

BSTAR

0.00066816

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Other satellites on launch #123 in the year 2023 (2023-08-20 UTC)

GAOFEN 12 04, 57654

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CZ-4C 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.
5 mins	2025-12-11 11:35:45.833Z	342.343° N	2025-12-11 11:37:45.833Z	292.517° NW	28.224°	2025-12-11 11:40:45.833Z	226.26° WSW
4 mins	2025-12-11 22:08:45.833Z	160.742° S	2025-12-11 22:09:45.833Z	147.604° SSE	42.264°	2025-12-11 22:12:45.833Z	349.759° N

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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-4C R/B, 57655 on other resources

View CZ-4C R/B, 57655 on Heavens-Above

View CZ-4C R/B, 57655 on Keep Track

View CZ-4C R/B, 57655 on Celestrak

View CZ-4C R/B, 57655 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-4C R/B, 57655

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2025-12-10T16:14:47.213Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #123 in the year 2023 (2023-08-20 UTC)

CZ-4C R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4C R/B, 57655 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago