CZ-6A DEB, 60778

Orbit data source: Space-Track

CZ-6A DEB, 60778 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/60778?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60778, 2024-140FD

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 (1 year 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

Small (<0.1 m²)

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

TLE from 15 hours ago

0 CZ-6A DEB
1 60778U 24140FD  25342.87588704  .00051349  00000-0  54890-2 0  9992
2 60778  89.0075 292.3366 0054015 154.9555 205.4312 14.87447168 70968

Epoch: 2025-12-08T21:01Z

TLE epoch observation values (Epoch: 2025-12-08T21:01:16.640Z)

Latitude

0.00004°

Longitude

-100.85137°

Altitude

643.179 km

Speed

7.518 km/s

True Right ascension

19h 29m 20s

True Declination

0° 00' 00"

Sunlit

Object was in daylight 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

10:13:27

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

640.478 km

Perigee altitude

565.063 km

Semi-major axis

6,980.907 km

Eccentricity

0.0054

Inclination

89.0075°

RAAN

292.3366°

Arg. of periapsis

154.9555°

True anomaly

205.16701°

Mean anomaly

205.4312°

Eccentric anomaly

205.29895°

Mean motion

3.72113 °/min

Orbital period

96.74 mins

BSTAR

0.005489

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

CZ-6A DEB, 61337 (Decayed)

CZ-6A DEB, 61298 (Decayed)

CZ-6A DEB, 61348 (Decayed)

CZ-6A DEB, 61356

CZ-6A DEB, 60893 (Decayed)

CZ-6A DEB, 64661

CZ-6A DEB, 64631

CZ-6A DEB, 61473 (Decayed)

CZ-6A DEB, 61413 (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	2025-12-09 21:21:00.006Z	184.588° SSW	2025-12-09 21:25:00.006Z	249.975° W	43.583°	2025-12-09 21:29:00.006Z	354.262° N
7 mins	2025-12-10 09:07:00.006Z	359.767° N	2025-12-10 09:10:00.006Z	298.484° NW	44.913°	2025-12-10 09:14:00.006Z	183.716° 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, 60778 on other resources

View CZ-6A DEB, 60778 on Heavens-Above

View CZ-6A DEB, 60778 on Keep Track

View CZ-6A DEB, 60778 on Celestrak

View CZ-6A DEB, 60778 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, 60778

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: 2025-12-08T21:01:16.640Z)

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, 60778 on other resources

Documentation

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