CZ-6A DEB, 60768

Orbit data source: Space-Track

CZ-6A DEB, 60768 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/60768?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60768, 2024-140ET

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, 0.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 CZ-6A DEB
1 60768U 24140ET  26171.26721652  .00002688  00000-0  54220-3 0  9996
2 60768  89.0936 277.4740 0109920 253.0563 105.8575 14.57434412 98441

Epoch: 2026-06-20T06:24Z

TLE epoch observation values (Epoch: 2026-06-20T06:24:47.507Z)

Latitude

-0.00011°

Longitude

-87.20824°

Altitude

726.634 km

Speed

7.48 km/s

True Right ascension

18h 29m 53s

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

07:14:23

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

776.152 km

Perigee altitude

620.582 km

Semi-major axis

7,076.504 km

Eccentricity

0.01099

Inclination

89.0936°

RAAN

277.474°

Arg. of periapsis

253.0563°

True anomaly

107.06453°

Mean anomaly

105.8575°

Eccentric anomaly

106.46148°

Mean motion

3.64599 °/min

Orbital period

98.74 mins

BSTAR

0.0005422

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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, 61344 (Decayed)

CZ-6A DEB, 60711

CZ-6A DEB, 61310 (Decayed)

QIANFAN-4, 60382

QIANFAN-5, 60383

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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 07:15:38.379Z	160.836° S	2026-06-21 07:18:38.379Z	106.025° ESE	41.365°	2026-06-21 07:23:38.379Z	6.452° NNE
4 mins	2026-06-21 08:56:38.379Z	262.437° W	2026-06-21 08:58:38.379Z	287.902° WNW	13.799°	2026-06-21 09:00:38.379Z	311.482° NW
8 mins	2026-06-21 19:15:38.379Z	6.859° NNE	2026-06-21 19:18:38.379Z	48.499° ENE	43.435°	2026-06-21 19:23:38.379Z	176.427° S

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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, 60768 on other resources

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View CZ-6A DEB, 60768 on Keep Track

View CZ-6A DEB, 60768 on Celestrak

View CZ-6A DEB, 60768 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, 60768

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-06-20T06:24:47.507Z)

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, 60768 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago