CZ-6A DEB, 60864

Orbit data source: Space-Track

CZ-6A DEB, 60864 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/60864?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60864, 2024-140JT

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

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago

0 CZ-6A DEB
1 60864U 24140JT  26118.51790142  .00001766  00000-0  61590-3 0  9996
2 60864  89.4114 309.8487 0017720 151.3230 208.8947 14.34909331 88364

Epoch: 2026-04-28T12:25Z

TLE epoch observation values (Epoch: 2026-04-28T12:25:46.682Z)

Latitude

-0.00002°

Longitude

-93.08788°

Altitude

789.549 km

Speed

7.453 km/s

True Right ascension

20h 39m 23s

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

03:42:10

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

784.966 km

Perigee altitude

759.625 km

Semi-major axis

7,150.433 km

Eccentricity

0.00177

Inclination

89.4114°

RAAN

309.8487°

Arg. of periapsis

151.323°

True anomaly

208.79677°

Mean anomaly

208.8947°

Eccentric anomaly

208.84572°

Mean motion

3.58959 °/min

Orbital period

100.29 mins

BSTAR

0.0006159

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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	2026-04-29 00:43:23.856Z	12.76° NNE	2026-04-29 00:47:23.856Z	72.104° E	38.813°	2026-04-29 00:52:23.856Z	165.637° S
4 mins	2026-04-29 02:26:23.856Z	300.552° NW	2026-04-29 02:27:23.856Z	286.915° WNW	15.348°	2026-04-29 02:30:23.856Z	249.866° W
5 mins	2026-04-29 12:01:23.856Z	104.089° ESE	2026-04-29 12:03:23.856Z	74.683° E	18.996°	2026-04-29 12:06:23.856Z	35.649° NE
8 mins	2026-04-29 13:39:23.856Z	205.944° SW	2026-04-29 13:43:23.856Z	279.281° WNW	34.805°	2026-04-29 13:47:23.856Z	341.876° N

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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, 60864 on other resources

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View CZ-6A DEB, 60864 on Gunter's Space Page

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CZ-6A DEB, 60864

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-04-28T12:25:46.682Z)

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, 60864 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago