CZ-6A DEB, 60764

Orbit data source: Space-Track

CZ-6A DEB, 60764 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/60764?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60764, 2024-140EP

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

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago

0 CZ-6A DEB
1 60764U 24140EP  26112.92919514  .00000271  00000-0  10570-3 0  9992
2 60764  88.9421 276.2099 0016671 288.5985  71.3398 14.26792422 88194

Epoch: 2026-04-22T22:18Z

TLE epoch observation values (Epoch: 2026-04-22T22:18:02.460Z)

Latitude

0°

Longitude

90.71607°

Altitude

801.722 km

Speed

7.455 km/s

True Right ascension

18h 24m 50s

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

00:45:49

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

811.38 km

Perigee altitude

787.449 km

Semi-major axis

7,177.551 km

Eccentricity

0.00167

Inclination

88.9421°

RAAN

276.2099°

Arg. of periapsis

288.5985°

True anomaly

71.52091°

Mean anomaly

71.3398°

Eccentric anomaly

71.43034°

Mean motion

3.56926 °/min

Orbital period

100.86 mins

BSTAR

0.0001057

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

CZ-6A DEB, 60629 (Decayed)

CZ-6A DEB, 61392 (Decayed)

CZ-6A DEB, 60851 (Decayed)

CZ-6A DEB, 61795 (Decayed)

CZ-6A DEB, 61433 (Decayed)

CZ-6A DEB, 61844 (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.
7 mins	2026-04-24 22:01:15.022Z	33.518° NE	2026-04-24 22:05:15.022Z	87.17° E	21.318°	2026-04-24 22:08:15.022Z	126.466° SE
8 mins	2026-04-24 23:42:15.022Z	339.103° N	2026-04-24 23:46:15.022Z	268.818° W	32.659°	2026-04-24 23:50:15.022Z	212.588° SW
8 mins	2026-04-25 11:01:15.022Z	169.013° S	2026-04-25 11:05:15.022Z	48.893° ENE	43.476°	2026-04-25 11:09:15.022Z	3.7° NNE

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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, 60764 on other resources

View CZ-6A DEB, 60764 on Heavens-Above

View CZ-6A DEB, 60764 on Keep Track

View CZ-6A DEB, 60764 on Celestrak

View CZ-6A DEB, 60764 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, 60764

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-04-22T22:18:02.460Z)

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, 60764 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago