CZ-6A R/B, 59344

Orbit data source: Space-Track

CZ-6A R/B, 59344 is space debris in SSO originally from a launch on Tue, 26 Mar 2024 UTC launched from the Taiyaun Space Center, China (TSC). 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/59344?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59344, 2024-058B

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

CZ-6A STAGE 2, YF-115

Mass

~6,000 kg wet, ~6,000 kg dry

Launch date (UTC)

2024-03-26 (2 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 5.5 m

Radar Cross Section

Large (>1 m²)

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

TLE from 2 days ago

0 CZ-6A R/B
1 59344U 24058B   26155.07162615  .00000065  00000-0  42530-4 0  9990
2 59344  98.7821 181.8539 0078103 192.6500 167.2722 14.28635768114091

Epoch: 2026-06-04T01:43Z

TLE epoch observation values (Epoch: 2026-06-04T01:43:08.499Z)

Latitude

-0.00007°

Longitude

-96.45265°

Altitude

853.908 km

Speed

7.397 km/s

True Right ascension

12h 07m 24s

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

10:48:23

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

849.457 km

Perigee altitude

737.433 km

Semi-major axis

7,171.582 km

Eccentricity

0.00781

Inclination

98.7821°

RAAN

181.8539°

Arg. of periapsis

192.65°

True anomaly

167.46752°

Mean anomaly

167.2722°

Eccentric anomaly

167.37005°

Mean motion

3.57372 °/min

Orbital period

100.74 mins

BSTAR

0.00004253

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Other satellites on launch #58 in the year 2024 (2024-03-26 UTC)

YUNHAI 3-02, 59343

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CZ-6A 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.
9 mins	2026-06-06 00:55:01.945Z	127.362° SE	2026-06-06 00:59:01.945Z	74.959° E	28.733°	2026-06-06 01:04:01.945Z	5.913° NNE
7 mins	2026-06-06 02:36:01.945Z	216.345° SW	2026-06-06 02:39:01.945Z	266.976° W	27.629°	2026-06-06 02:43:01.945Z	321.751° NNW
9 mins	2026-06-06 14:48:01.945Z	11.316° NNE	2026-06-06 14:53:01.945Z	288.297° WNW	44.605°	2026-06-06 14:57:01.945Z	199.746° SSW
5 mins	2026-06-07 00:30:01.945Z	89.104° E	2026-06-07 00:32:01.945Z	61.453° ENE	18.694°	2026-06-07 00:35:01.945Z	24.015° NE

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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-6A R/B, 59344 on other resources

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View CZ-6A R/B, 59344 on Keep Track

View CZ-6A R/B, 59344 on Celestrak

View CZ-6A R/B, 59344 on Gunter's Space Page

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CZ-6A R/B, 59344

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: 2026-06-04T01:43:08.499Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #58 in the year 2024 (2024-03-26 UTC)

CZ-6A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-6A R/B, 59344 on other resources

Documentation

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