CZ-6A DEB, 60713

Orbit data source: Space-Track

CZ-6A DEB, 60713 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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https://www.satcat.com/sats-embedded/60713?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60713, 2024-140DS

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 (1 year 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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago

0 CZ-6A DEB
1 60713U 24140DS  25354.27315008  .00000180  00000-0  78537-4 0  9996
2 60713  89.0165 295.8351 0049335  29.9420 330.4574 14.18947377 70229

Epoch: 2025-12-20T06:33Z

TLE epoch observation values (Epoch: 2025-12-20T06:33:20.166Z)

Latitude

-0.0001°

Longitude

108.39875°

Altitude

801.07 km

Speed

7.469 km/s

True Right ascension

19h 43m 20s

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

00:58:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

861.408 km

Perigee altitude

790.326 km

Semi-major axis

7,204.004 km

Eccentricity

0.00493

Inclination

89.0165°

RAAN

295.8351°

Arg. of periapsis

29.942°

True anomaly

330.17715°

Mean anomaly

330.4574°

Eccentric anomaly

330.31742°

Mean motion

3.54962 °/min

Orbital period

101.42 mins

BSTAR

0.000078537

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

CZ-6A DEB, 60743 (Decayed)

CZ-6A DEB, 61344 (Decayed)

CZ-6A DEB, 61342 (Decayed)

CZ-6A DEB, 61820 (Decayed)

CZ-6A DEB, 60835 (Decayed)

QIANFAN-11, 60389

QIANFAN-10, 60388

QIANFAN-14, 60392

CZ-6A DEB, 60862 (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.
10 mins	2025-12-21 08:31:17.062Z	2.825° NNE	2025-12-21 08:36:17.062Z	158.987° S	44.008°	2025-12-21 08:41:17.062Z	180.093° SSW
8 mins	2025-12-21 19:55:17.062Z	136.089° SSE	2025-12-21 19:58:17.062Z	91.446° ESE	28.537°	2025-12-21 20:03:17.062Z	18.809° NNE
7 mins	2025-12-21 21:37:17.062Z	232.694° WSW	2025-12-21 21:40:17.062Z	279.018° WNW	23.969°	2025-12-21 21:44:17.062Z	332.134° NNW

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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, 60713 on other resources

View CZ-6A DEB, 60713 on Heavens-Above

View CZ-6A DEB, 60713 on Keep Track

View CZ-6A DEB, 60713 on Celestrak

View CZ-6A DEB, 60713 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, 60713

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 19 hours ago

TLE from 19 hours ago

TLE epoch observation values (Epoch: 2025-12-20T06:33:20.166Z)

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, 60713 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 19 hours ago