CZ-6A DEB, 60855

Orbit data source: Space-Track

CZ-6A DEB, 60855 is space debris in LEO originally from a launch on Tue, 06 Aug 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/60855?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60855, 2024-140JJ

Orbit

LEO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2024-08-06 (2 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.2 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 22 hours ago

TLE from 22 hours ago

0 CZ-6A DEB
1 60855U 24140JJ  26113.39468552  .00000555  00000-0  27615-3 0  9999
2 60855  89.0117 282.7866 0073391  17.9462 342.4290 14.14271443 87171

Epoch: 2026-04-23T09:28Z

TLE epoch observation values (Epoch: 2026-04-23T09:28:20.828Z)

Latitude

-0.00008°

Longitude

-70.74257°

Altitude

797.325 km

Speed

7.481 km/s

True Right ascension

18h 51m 08s

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

14:39:11

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

894.738 km

Perigee altitude

788.763 km

Semi-major axis

7,219.888 km

Eccentricity

0.00734

Inclination

89.0117°

RAAN

282.7866°

Arg. of periapsis

17.9462°

True anomaly

342.17287°

Mean anomaly

342.429°

Eccentric anomaly

342.30116°

Mean motion

3.53792 °/min

Orbital period

101.75 mins

BSTAR

0.00027615

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Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)

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CZ-6A 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.
9 mins	2026-04-24 11:03:16.519Z	149.225° SSE	2026-04-24 11:08:16.519Z	70.146° E	32.508°	2026-04-24 11:12:16.519Z	16.331° NNE
6 mins	2026-04-24 12:47:16.519Z	242.499° WSW	2026-04-24 12:50:16.519Z	286.815° WNW	20.335°	2026-04-24 12:53:16.519Z	324.78° NNW
9 mins	2026-04-24 23:25:16.519Z	5.275° NNE	2026-04-24 23:29:16.519Z	111.839° ESE	44.481°	2026-04-24 23:34:16.519Z	177.728° 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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View CZ-6A DEB, 60855 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-6A DEB, 60855

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 22 hours ago

TLE from 22 hours ago

TLE epoch observation values (Epoch: 2026-04-23T09:28:20.828Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)

CZ-6A DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-6A DEB, 60855 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 22 hours ago