CZ-6A DEB, 60785

Orbit data source: Space-Track

CZ-6A DEB, 60785 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/60785?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60785, 2024-140FL

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: 15 hours ago

TLE from 15 hours ago

0 CZ-6A DEB
1 60785U 24140FL  26171.29569308  .00000201  00000-0  48140-4 0  9990
2 60785  88.9913 269.9267 0095441 288.0938  70.9889 14.47028964 97909

Epoch: 2026-06-20T07:05Z

TLE epoch observation values (Epoch: 2026-06-20T07:05:47.882Z)

Latitude

-0.00001°

Longitude

-105.03517°

Altitude

716.922 km

Speed

7.508 km/s

True Right ascension

17h 59m 42s

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

08:33:27

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

800.144 km

Perigee altitude

664.418 km

Semi-major axis

7,110.418 km

Eccentricity

0.00954

Inclination

88.9913°

RAAN

269.9267°

Arg. of periapsis

288.0938°

True anomaly

72.0269°

Mean anomaly

70.9889°

Eccentric anomaly

71.5075°

Mean motion

3.61993 °/min

Orbital period

99.45 mins

BSTAR

0.00004814

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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)

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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.
9 mins	2026-06-21 06:26:29.981Z	151.081° SSE	2026-06-21 06:31:29.981Z	69.523° E	33.067°	2026-06-21 06:35:29.981Z	15.319° NNE
6 mins	2026-06-21 08:08:29.981Z	245.912° WSW	2026-06-21 08:10:29.981Z	275.15° WNW	19.636°	2026-06-21 08:14:29.981Z	327.165° NNW
8 mins	2026-06-21 18:32:29.981Z	14.231° NNE	2026-06-21 18:36:29.981Z	106.744° ESE	39.897°	2026-06-21 18:40:29.981Z	165.572° S
4 mins	2026-06-21 20:13:29.981Z	305.755° NW	2026-06-21 20:15:29.981Z	279.435° WNW	15.471°	2026-06-21 20:17:29.981Z	254.962° W

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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, 60785 on other resources

View CZ-6A DEB, 60785 on Heavens-Above

View CZ-6A DEB, 60785 on Keep Track

View CZ-6A DEB, 60785 on Celestrak

View CZ-6A DEB, 60785 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, 60785

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: 2026-06-20T07:05:47.882Z)

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, 60785 on other resources

Documentation

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