CZ-6A DEB, 60626

Orbit data source: Space-Track

CZ-6A DEB, 60626 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/60626?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60626, 2024-140AB

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: 10 hours ago

TLE from 10 hours ago

0 CZ-6A DEB
1 60626U 24140AB  26171.44973973  .00003182  00000-0  28386-3 0  9998
2 60626  89.0196 268.2888 0211277 160.2659 200.6900 14.80042661100613

Epoch: 2026-06-20T10:47Z

TLE epoch observation values (Epoch: 2026-06-20T10:47:37.512Z)

Latitude

-0.00006°

Longitude

-162.2817°

Altitude

771.242 km

Speed

7.394 km/s

True Right ascension

17h 53m 09s

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

07:22:40

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

774.035 km

Perigee altitude

478.071 km

Semi-major axis

7,004.19 km

Eccentricity

0.02113

Inclination

89.0196°

RAAN

268.2888°

Arg. of periapsis

160.2659°

True anomaly

199.85529°

Mean anomaly

200.69°

Eccentric anomaly

200.27061°

Mean motion

3.7026 °/min

Orbital period

97.23 mins

BSTAR

0.00028386

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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.
8 mins	2026-06-21 06:22:54.255Z	151.883° SSE	2026-06-21 06:26:54.255Z	92.983° ESE	33.295°	2026-06-21 06:30:54.255Z	17.318° NNE
4 mins	2026-06-21 08:02:54.255Z	252.079° W	2026-06-21 08:04:54.255Z	283.234° WNW	17.621°	2026-06-21 08:06:54.255Z	312.555° NW
4 mins	2026-06-21 18:13:54.255Z	48.462° ENE	2026-06-21 18:14:54.255Z	75.642° E	25.626°	2026-06-21 18:17:54.255Z	143.985° SSE

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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, 60626 on other resources

View CZ-6A DEB, 60626 on Heavens-Above

View CZ-6A DEB, 60626 on Keep Track

View CZ-6A DEB, 60626 on Celestrak

View CZ-6A DEB, 60626 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, 60626

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-06-20T10:47:37.512Z)

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, 60626 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago