CZ-6A DEB, 60761

Orbit data source: Space-Track

CZ-6A DEB, 60761 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/60761?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60761, 2024-140EL

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: 15 hours ago

TLE from 15 hours ago

0 CZ-6A DEB
1 60761U 24140EL  26171.28263720  .00024442  00000-0  25783-2 0  9991
2 60761  89.0029 268.8044 0058153 190.6111 169.3895 14.87935771 99655

Epoch: 2026-06-20T06:46Z

TLE epoch observation values (Epoch: 2026-06-20T06:46:59.854Z)

Latitude

-0°

Longitude

-101.44448°

Altitude

647.464 km

Speed

7.512 km/s

True Right ascension

17h 55m 13s

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

08:43:02

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

641.828 km

Perigee altitude

560.653 km

Semi-major axis

6,979.378 km

Eccentricity

0.00582

Inclination

89.0029°

RAAN

268.8044°

Arg. of periapsis

190.6111°

True anomaly

169.51133°

Mean anomaly

169.3895°

Eccentric anomaly

169.4505°

Mean motion

3.72236 °/min

Orbital period

96.71 mins

BSTAR

0.0025783

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

CZ-6A DEB, 61384 (Decayed)

CZ-6A DEB, 60777 (Decayed)

CZ-6A DEB, 61344 (Decayed)

CZ-6A DEB, 61310 (Decayed)

CZ-6A DEB, 61285 (Decayed)

CZ-6A DEB, 61391 (Decayed)

CZ-6A DEB, 61343 (Decayed)

CZ-6A DEB, 61802 (Decayed)

CZ-6A DEB, 60851 (Decayed)

CZ-6A DEB, 60869 (Decayed)

CZ-6A DEB, 61473 (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.
8 mins	2026-06-21 07:06:02.640Z	185.802° SSW	2026-06-21 07:10:02.640Z	231.092° WSW	42.107°	2026-06-21 07:14:02.640Z	352.431° N
6 mins	2026-06-21 18:53:02.640Z	357.168° N	2026-06-21 18:55:02.640Z	327.21° NNW	44.081°	2026-06-21 18:59:02.640Z	185.561° SSW

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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, 60761 on other resources

View CZ-6A DEB, 60761 on Heavens-Above

View CZ-6A DEB, 60761 on Keep Track

View CZ-6A DEB, 60761 on Celestrak

View CZ-6A DEB, 60761 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, 60761

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2026-06-20T06:46:59.854Z)

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, 60761 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 15 hours ago