CZ-4C R/B, 59729

Orbit data source: Space-Track

CZ-4C R/B, 59729 is space debris in SSO originally from a launch on Sat, 11 May 2024 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/59729?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59729, 2024-089B

Orbit

SSO

Last TLE update

9 hours ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

CZ-4 STAGE 3, Unknown motor

Mass

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

Launch date (UTC)

2024-05-11 (1 year ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history

TLE from 9 hours ago

0 CZ-4C R/B
1 59729U 24089B   25224.56058419  .00006983  00000-0  25271-3 0  9994
2 59729  97.7379 250.6776 0084127 249.4958 109.7235 15.25418872 69502

Epoch: 2025-08-12T13:27Z

TLE epoch observation values (Epoch: 2025-08-12T13:27:14.474Z)

Latitude

0.00001°

Longitude

87.61582°

Altitude

512.547 km

Speed

7.596 km/s

True Right ascension

16h 42m 42s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-5.36346°

Longitude

-92.7367°

Altitude

466.814 km

Speed

7.647 km/s

Apparent Right ascension

03h 00m 14s

Apparent Declination

-24° 58' 31"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:34:32

Azimuth

284.996° WNW

Elevation

-56.136°

Doppler factor

Orbital elements

Apogee altitude

544.251 km

Perigee altitude

428.751 km

Semi-major axis

6,864.638 km

Eccentricity

0.00841

Inclination

97.7379°

RAAN

250.6776°

Arg. of periapsis

249.4958°

True anomaly

110.62772°

Mean anomaly

109.7235°

Eccentric anomaly

110.17593°

Mean motion

3.81607 °/min

Orbital period

94.34 mins

BSTAR

0.00025271

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Other satellites on launch #89 in the year 2024 (2024-05-11 UTC)

SHIYAN 23 (SY-23), 59728

CZ-4C R/B Visibility forecast

Observer location: undefined°, undefined°
Set Observer location

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	2025-08-13 02:11:34.868Z	200.383° SSW	2025-08-13 02:13:34.868Z	270.696° WNW	36.079°	2025-08-13 02:16:34.868Z	332.773° NNW
4 mins	2025-08-13 15:13:34.868Z	336.207° NNW	2025-08-13 15:15:34.868Z	276.422° WNW	28.972°	2025-08-13 15:17:34.868Z	231.041° WSW

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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Check out CZ-4C R/B, 59729 on other resources

View CZ-4C R/B, 59729 on Heavens-Above

View CZ-4C R/B, 59729 on Keep Track

View CZ-4C R/B, 59729 on Celestrak

View CZ-4C R/B, 59729 on Gunter's Space Page

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