CZ-6A DEB, 60710

Orbit data source: Space-Track

CZ-6A DEB, 60710 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/60710?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60710, 2024-140DP

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, 0.3 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago

0 CZ-6A DEB
1 60710U 24140DP  26118.75989771  .00000279  00000-0  12426-3 0  9992
2 60710  89.2037 295.6024 0042469 339.5316  20.4170 14.19827678 88629

Epoch: 2026-04-28T18:14Z

TLE epoch observation values (Epoch: 2026-04-28T18:14:15.162Z)

Latitude

-0.00002°

Longitude

165.30863°

Altitude

800.326 km

Speed

7.468 km/s

True Right ascension

19h 42m 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

10:58:53

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

853.468 km

Perigee altitude

792.304 km

Semi-major axis

7,201.023 km

Eccentricity

0.00425

Inclination

89.2037°

RAAN

295.6024°

Arg. of periapsis

339.5316°

True anomaly

20.58762°

Mean anomaly

20.417°

Eccentric anomaly

20.50222°

Mean motion

3.55183 °/min

Orbital period

101.36 mins

BSTAR

0.00012426

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

CZ-6A DEB, 61460 (Decayed)

CZ-6A DEB, 60869 (Decayed)

CZ-6A DEB, 61812

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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	2026-04-29 11:16:54.691Z	130.602° SE	2026-04-29 11:20:54.691Z	72.743° E	24.869°	2026-04-29 11:24:54.691Z	23.159° NE
7 mins	2026-04-29 12:58:54.691Z	225.509° WSW	2026-04-29 13:01:54.691Z	277.752° WNW	28.643°	2026-04-29 13:05:54.691Z	335.251° NNW
9 mins	2026-04-29 23:34:54.691Z	17.708° NNE	2026-04-29 23:38:54.691Z	85.629° E	37.241°	2026-04-29 23:43:54.691Z	160.882° S
5 mins	2026-04-30 01:17:54.691Z	311.152° NW	2026-04-30 01:19:54.691Z	283.817° WNW	19.373°	2026-04-30 01:22:54.691Z	245.97° WSW

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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, 60710 on other resources

View CZ-6A DEB, 60710 on Heavens-Above

View CZ-6A DEB, 60710 on Keep Track

View CZ-6A DEB, 60710 on Celestrak

View CZ-6A DEB, 60710 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, 60710

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2026-04-28T18:14:15.162Z)

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, 60710 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 9 hours ago