CZ-6A DEB, 60681

Orbit data source: Space-Track

CZ-6A DEB, 60681 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/60681?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60681, 2024-140CJ

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: 13 hours ago

TLE from 13 hours ago

0 CZ-6A DEB
1 60681U 24140CJ  26171.31311333  .00000331  00000-0  22703-3 0  9991
2 60681  88.9960 277.7078 0180245 276.1304  81.9360 13.90220456 94477

Epoch: 2026-06-20T07:30Z

TLE epoch observation values (Epoch: 2026-06-20T07:30:52.991Z)

Latitude

-0.00008°

Longitude

-103.54253°

Altitude

914.729 km

Speed

7.403 km/s

True Right ascension

18h 30m 49s

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

07:23:29

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,056.484 km

Perigee altitude

793.218 km

Semi-major axis

7,302.988 km

Eccentricity

0.01802

Inclination

88.996°

RAAN

277.7078°

Arg. of periapsis

276.1304°

True anomaly

83.98708°

Mean anomaly

81.936°

Eccentric anomaly

82.96094°

Mean motion

3.4777 °/min

Orbital period

103.52 mins

BSTAR

0.00022703

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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 06:06:43.008Z	113.537° SE	2026-06-21 06:10:43.008Z	72.441° E	17.931°	2026-06-21 06:14:43.008Z	32.829° NE
11 mins	2026-06-21 07:48:43.008Z	191.498° SSW	2026-06-21 07:53:43.008Z	284.882° WNW	42.415°	2026-06-21 07:59:43.008Z	353.407° N
10 mins	2026-06-21 18:40:43.008Z	22.859° NE	2026-06-21 18:44:43.008Z	77.164° E	33.7°	2026-06-21 18:50:43.008Z	153.89° 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, 60681 on other resources

View CZ-6A DEB, 60681 on Heavens-Above

View CZ-6A DEB, 60681 on Keep Track

View CZ-6A DEB, 60681 on Celestrak

View CZ-6A DEB, 60681 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, 60681

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 13 hours ago

TLE from 13 hours ago

TLE epoch observation values (Epoch: 2026-06-20T07:30:52.991Z)

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, 60681 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 13 hours ago