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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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 (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

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago

0 CZ-6A DEB
1 60778U 24140FD  26054.04557521  .00063936  00000-0  53318-2 0  9994
2 60778  89.0023 282.6853 0041159 244.6753 115.0214 14.97644138 82323

Epoch: 2026-02-23T01:05Z

TLE epoch observation values (Epoch: 2026-02-23T01:05:37.698Z)

Latitude

-0.00006°

Longitude

113.33313°

Altitude

589.543 km

Speed

7.559 km/s

True Right ascension

18h 50m 44s

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

00:12:35

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

599.62 km

Perigee altitude

542.416 km

Semi-major axis

6,949.155 km

Eccentricity

0.00412

Inclination

89.0023°

RAAN

282.6853°

Arg. of periapsis

244.6753°

True anomaly

115.44785°

Mean anomaly

115.0214°

Eccentric anomaly

115.23472°

Mean motion

3.74667 °/min

Orbital period

96.09 mins

BSTAR

0.0053318

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

QIANFAN-10, 60388

QIANFAN-14, 60392

QIANFAN-11, 60389

CZ-6A DEB, 61800 (Decayed)

CZ-6A DEB, 64632

CZ-6A DEB, 61343 (Decayed)

CZ-6A DEB, 61342 (Decayed)

CZ-6A DEB, 61495 (Decayed)

CZ-6A DEB, 61844 (Decayed)

CZ-6A DEB, 61457 (Decayed)

CZ-6A DEB, 61407 (Decayed)

CZ-6A DEB, 60888 (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.
7 mins	2026-02-24 03:19:01.016Z	6.377° NNE	2026-02-24 03:23:01.016Z	128.534° SE	42.457°	2026-02-24 03:26:01.016Z	173.41° S
6 mins	2026-02-24 15:43:01.016Z	191.575° SSW	2026-02-24 15:45:01.016Z	234.779° WSW	42.159°	2026-02-24 15:49:01.016Z	352.777° N

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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: 20 hours ago

TLE from 20 hours ago

TLE epoch observation values (Epoch: 2026-02-23T01:05:37.698Z)

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: 20 hours ago