CZ-6A DEB, 60678

Orbit data source: Space-Track

CZ-6A DEB, 60678 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/60678?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60678, 2024-140CF

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, 0.3 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago

0 CZ-6A DEB
1 60678U 24140CF  26118.82287808  .00000425  00000-0  11789-3 0  9999
2 60678  88.9035 270.3632 0075026 115.8409 245.0557 14.42970242 90500

Epoch: 2026-04-28T19:44Z

TLE epoch observation values (Epoch: 2026-04-28T19:44:56.666Z)

Latitude

0.00005°

Longitude

117.33442°

Altitude

774.671 km

Speed

7.455 km/s

True Right ascension

18h 01m 27s

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

11:00:25

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

799.067 km

Perigee altitude

692.174 km

Semi-major axis

7,123.757 km

Eccentricity

0.0075

Inclination

88.9035°

RAAN

270.3632°

Arg. of periapsis

115.8409°

True anomaly

244.27926°

Mean anomaly

245.0557°

Eccentric anomaly

244.66717°

Mean motion

3.60977 °/min

Orbital period

99.73 mins

BSTAR

0.00011789

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

CZ-6A DEB, 61460 (Decayed)

CZ-6A DEB, 60869 (Decayed)

CZ-6A DEB, 61812

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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.
4 mins	2026-04-29 09:13:26.502Z	101.198° ESE	2026-04-29 09:15:26.502Z	75.708° E	13.857°	2026-04-29 09:17:26.502Z	50.011° ENE
8 mins	2026-04-29 10:51:26.502Z	197.912° SSW	2026-04-29 10:54:26.502Z	255.64° W	39.886°	2026-04-29 10:59:26.502Z	350.524° N
5 mins	2026-04-29 21:19:26.502Z	54.647° ENE	2026-04-29 21:21:26.502Z	86.763° E	18.263°	2026-04-29 21:24:26.502Z	126.371° SE
7 mins	2026-04-29 22:58:26.502Z	331.957° NNW	2026-04-29 23:01:26.502Z	264.876° W	31.361°	2026-04-29 23:05:26.502Z	209.863° SW

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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, 60678 on other resources

View CZ-6A DEB, 60678 on Heavens-Above

View CZ-6A DEB, 60678 on Keep Track

View CZ-6A DEB, 60678 on Celestrak

View CZ-6A DEB, 60678 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, 60678

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-04-28T19:44:56.666Z)

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, 60678 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago