CZ-6A DEB, 60859

Orbit data source: Space-Track

CZ-6A DEB, 60859 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/60859?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60859, 2024-140JN

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, 0.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago

0 CZ-6A DEB
1 60859U 24140JN  26171.44122416  .00001402  00000-0  41839-3 0  9995
2 60859  88.5659 235.8660 0062846 340.8077  19.0757 14.41373601 96965

Epoch: 2026-06-20T10:35Z

TLE epoch observation values (Epoch: 2026-06-20T10:35:21.767Z)

Latitude

-0.00003°

Longitude

168.3695°

Altitude

714.706 km

Speed

7.52 km/s

True Right ascension

15h 43m 27s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

07:23:00

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

795.69 km

Perigee altitude

706.084 km

Semi-major axis

7,129.024 km

Eccentricity

0.00628

Inclination

88.5659°

RAAN

235.866°

Arg. of periapsis

340.8077°

True anomaly

19.31282°

Mean anomaly

19.0757°

Eccentric anomaly

19.19408°

Mean motion

3.60577 °/min

Orbital period

99.84 mins

BSTAR

0.00041839

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

CZ-6A DEB, 60882

CZ-6A DEB, 61384 (Decayed)

CZ-6A DEB, 60744 (Decayed)

CZ-6A DEB, 60849

CZ-6A DEB, 60885

CZ-6A DEB, 61344 (Decayed)

CZ-6A DEB, 60711

CZ-6A DEB, 60799

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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.
8 mins	2026-06-21 05:02:14.299Z	192.879° SSW	2026-06-21 05:06:14.299Z	289.391° WNW	41.423°	2026-06-21 05:10:14.299Z	351.437° N
6 mins	2026-06-21 15:31:14.299Z	47.728° ENE	2026-06-21 15:33:14.299Z	76.97° E	20.565°	2026-06-21 15:37:14.299Z	128.806° SE
8 mins	2026-06-21 17:10:14.299Z	337.167° NNW	2026-06-21 17:13:14.299Z	286.206° WNW	33.456°	2026-06-21 17:18:14.299Z	208.696° SW

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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 DEB, 60859 on other resources

View CZ-6A DEB, 60859 on Heavens-Above

View CZ-6A DEB, 60859 on Keep Track

View CZ-6A DEB, 60859 on Celestrak

View CZ-6A DEB, 60859 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, 60859

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-06-20T10:35:21.767Z)

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, 60859 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago