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 (3 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 2.5 m

Radar Cross Section

14.536 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago

0 CZ-4C R/B
1 57655U 23123B   26097.22213470  .00018859  00000-0  48172-3 0  9990
2 57655  97.9706  81.3659 0058104 327.7038  32.0652 15.37771345146167

Epoch: 2026-04-07T05:19Z

TLE epoch observation values (Epoch: 2026-04-07T05:19:52.438Z)

Latitude

-0.00001°

Longitude

165.89546°

Altitude

422.222 km

Speed

7.677 km/s

True Right ascension

05h 25m 27s

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

00:23:15

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

489.341 km

Perigee altitude

409.996 km

Semi-major axis

6,827.805 km

Eccentricity

0.00581

Inclination

97.9706°

RAAN

81.3659°

Arg. of periapsis

327.7038°

True anomaly

32.42086°

Mean anomaly

32.0652°

Eccentric anomaly

32.24281°

Mean motion

3.84699 °/min

Orbital period

93.58 mins

BSTAR

0.00048172

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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	2026-04-07 22:38:35.643Z	147.321° SSE	2026-04-07 22:41:35.643Z	46.981° ENE	36.064°	2026-04-07 22:43:35.643Z	2.478° NNE
5 mins	2026-04-08 11:34:35.643Z	29.109° NE	2026-04-08 11:36:35.643Z	90.547° ESE	39.422°	2026-04-08 11:39:35.643Z	177.442° 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-4C R/B, 57655 on other resources

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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: 13 hours ago

TLE from 13 hours ago

TLE epoch observation values (Epoch: 2026-04-07T05:19:52.438Z)

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: 13 hours ago