CZ-6A DEB, 60779

Orbit data source: Space-Track

CZ-6A DEB, 60779 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/60779?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60779, 2024-140FE

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: 16 hours ago

TLE from 16 hours ago

0 CZ-6A DEB
1 60779U 24140FE  26171.18836387  .00017380  00000-0  22034-2 0  9993
2 60779  88.9705 265.7553 0079662 201.3624 158.4269 14.79404286 98972

Epoch: 2026-06-20T04:31Z

TLE epoch observation values (Epoch: 2026-06-20T04:31:14.638Z)

Latitude

-0.00002°

Longitude

-70.46226°

Altitude

686.34 km

Speed

7.485 km/s

True Right ascension

17h 43m 01s

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

07:19:34

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

683.884 km

Perigee altitude

572.259 km

Semi-major axis

7,006.209 km

Eccentricity

0.00797

Inclination

88.9705°

RAAN

265.7553°

Arg. of periapsis

201.3624°

True anomaly

158.75946°

Mean anomaly

158.4269°

Eccentric anomaly

158.59349°

Mean motion

3.701 °/min

Orbital period

97.27 mins

BSTAR

0.0022034

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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)

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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 06:36:49.024Z	170.452° S	2026-06-21 06:40:49.024Z	61.955° ENE	43.762°	2026-06-21 06:44:49.024Z	3.284° NNE
6 mins	2026-06-21 18:26:49.024Z	9.685° NNE	2026-06-21 18:29:49.024Z	112.473° ESE	42.73°	2026-06-21 18:32:49.024Z	171.745° S

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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, 60779 on other resources

View CZ-6A DEB, 60779 on Heavens-Above

View CZ-6A DEB, 60779 on Keep Track

View CZ-6A DEB, 60779 on Celestrak

View CZ-6A DEB, 60779 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, 60779

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2026-06-20T04:31:14.638Z)

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, 60779 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 16 hours ago