CZ-6A DEB, 60850

Orbit data source: Space-Track

CZ-6A DEB, 60850 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/60850?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60850, 2024-140JD

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: 18 hours ago

TLE from 18 hours ago

0 CZ-6A DEB
1 60850U 24140JD  26171.21856746  .00000344  00000-0  14259-3 0  9991
2 60850  88.8625 262.6301 0026740 140.6405 219.6737 14.24034650 95993

Epoch: 2026-06-20T05:14Z

TLE epoch observation values (Epoch: 2026-06-20T05:14:44.228Z)

Latitude

-0.00005°

Longitude

-84.49053°

Altitude

829.621 km

Speed

7.43 km/s

True Right ascension

17h 30m 31s

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

10:20:33

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

827.904 km

Perigee altitude

789.469 km

Semi-major axis

7,186.823 km

Eccentricity

0.00267

Inclination

88.8625°

RAAN

262.6301°

Arg. of periapsis

140.6405°

True anomaly

219.47858°

Mean anomaly

219.6737°

Eccentric anomaly

219.57609°

Mean motion

3.56236 °/min

Orbital period

101.06 mins

BSTAR

0.00014259

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

CZ-6A DEB, 61384 (Decayed)

CZ-6A DEB, 61344 (Decayed)

CZ-6A DEB, 60710

CZ-6A DEB, 60782 (Decayed)

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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 06:40:18.449Z	185.646° SSW	2026-06-21 06:43:18.449Z	222.771° SW	43.589°	2026-06-21 06:48:18.449Z	355.518° N
6 mins	2026-06-21 17:16:18.449Z	46.996° ENE	2026-06-21 17:18:18.449Z	74.941° E	19.441°	2026-06-21 17:22:18.449Z	126.747° SE
8 mins	2026-06-21 18:56:18.449Z	340.693° N	2026-06-21 19:00:18.449Z	266.061° W	33.975°	2026-06-21 19:04:18.449Z	209.46° 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, 60850 on other resources

View CZ-6A DEB, 60850 on Heavens-Above

View CZ-6A DEB, 60850 on Keep Track

View CZ-6A DEB, 60850 on Celestrak

View CZ-6A DEB, 60850 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, 60850

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 18 hours ago

TLE from 18 hours ago

TLE epoch observation values (Epoch: 2026-06-20T05:14:44.228Z)

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, 60850 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 18 hours ago