CZ-6A DEB, 60625

Orbit data source: Space-Track

CZ-6A DEB, 60625 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/60625?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60625, 2024-140AA

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, 0.2 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 CZ-6A DEB
1 60625U 24140AA  26171.33569161  .00002944  00000-0  76133-3 0  9993
2 60625  88.9958 271.0311 0059764 330.5452  29.2390 14.48631060 98371

Epoch: 2026-06-20T08:03Z

TLE epoch observation values (Epoch: 2026-06-20T08:03:23.755Z)

Latitude

-0.00001°

Longitude

-118.36966°

Altitude

696.201 km

Speed

7.527 km/s

True Right ascension

18h 04m 07s

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

07:23:32

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

769.497 km

Perigee altitude

684.57 km

Semi-major axis

7,105.17 km

Eccentricity

0.00598

Inclination

88.9958°

RAAN

271.0311°

Arg. of periapsis

330.5452°

True anomaly

29.57571°

Mean anomaly

29.239°

Eccentric anomaly

29.40713°

Mean motion

3.62394 °/min

Orbital period

99.34 mins

BSTAR

0.00076133

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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.
7 mins	2026-06-21 07:23:45.667Z	196.925° SSW	2026-06-21 07:26:45.667Z	264.583° W	40.736°	2026-06-21 07:30:45.667Z	348.676° N
6 mins	2026-06-21 17:48:45.667Z	45.797° ENE	2026-06-21 17:51:45.667Z	88.212° E	18.332°	2026-06-21 17:54:45.667Z	124.814° SE
7 mins	2026-06-21 19:27:45.667Z	338.878° N	2026-06-21 19:30:45.667Z	280.326° WNW	35.423°	2026-06-21 19:34:45.667Z	209.378° 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, 60625 on other resources

View CZ-6A DEB, 60625 on Heavens-Above

View CZ-6A DEB, 60625 on Keep Track

View CZ-6A DEB, 60625 on Celestrak

View CZ-6A DEB, 60625 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, 60625

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-06-20T08:03:23.755Z)

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, 60625 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago