CZ-6A DEB, 61080

Orbit data source: Space-Track

CZ-6A DEB, 61080 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/61080?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61080, 2024-140MW

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, 0.2 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago

0 CZ-6A DEB
1 61080U 24140MW  25311.98148058  .00009232  00000-0  29194-2 0  9994
2 61080  89.2478 312.1030 0018249 278.3636  81.5496 14.40018833 63008

Epoch: 2025-11-07T23:33Z

TLE epoch observation values (Epoch: 2025-11-07T23:33:19.922Z)

Latitude

-0.00003°

Longitude

-88.64766°

Altitude

759.628 km

Speed

7.475 km/s

True Right ascension

20h 48m 24s

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

06:30:31

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

768.375 km

Perigee altitude

742.34 km

Semi-major axis

7,133.495 km

Eccentricity

0.00182

Inclination

89.2478°

RAAN

312.103°

Arg. of periapsis

278.3636°

True anomaly

81.75652°

Mean anomaly

81.5496°

Eccentric anomaly

81.65305°

Mean motion

3.60238 °/min

Orbital period

99.93 mins

BSTAR

0.0029194

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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, 61413 (Decayed)

CZ-6A DEB, 61143

CZ-6A DEB, 60806 (Decayed)

CZ-6A DEB, 61324 (Decayed)

CZ-6A DEB, 61328 (Decayed)

CZ-6A DEB, 61122

CZ-6A DEB, 61271 (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	2025-11-08 11:48:33.581Z	22.307° NNE	2025-11-08 11:52:33.581Z	81.134° E	29.868°	2025-11-08 11:56:33.581Z	146.226° SSE
6 mins	2025-11-08 13:29:33.581Z	324.893° NNW	2025-11-08 13:32:33.581Z	279.826° WNW	22.618°	2025-11-08 13:35:33.581Z	236.344° WSW
8 mins	2025-11-09 00:41:33.581Z	185.098° SSW	2025-11-09 00:45:33.581Z	296.459° NW	43.873°	2025-11-09 00:49:33.581Z	354.222° N

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, 61080 on other resources

View CZ-6A DEB, 61080 on Heavens-Above

View CZ-6A DEB, 61080 on Keep Track

View CZ-6A DEB, 61080 on Celestrak

View CZ-6A DEB, 61080 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, 61080

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2025-11-07T23:33:19.922Z)

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, 61080 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago