CZ-6A DEB, 61360

Orbit data source: Space-Track

CZ-6A DEB, 61360 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/61360?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61360, 2024-140VZ

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: 8 hours ago

TLE from 8 hours ago

0 CZ-6A DEB
1 61360U 24140VZ  26118.44890689  .00000929  00000-0  42855-3 0  9990
2 61360  89.0118 281.5975 0049284 355.0564   5.0132 14.19605006 85351

Epoch: 2026-04-28T10:46Z

TLE epoch observation values (Epoch: 2026-04-28T10:46:25.555Z)

Latitude

-0.00003°

Longitude

-96.43304°

Altitude

794.363 km

Speed

7.475 km/s

True Right ascension

18h 46m 23s

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

02:16:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

859.134 km

Perigee altitude

788.147 km

Semi-major axis

7,201.778 km

Eccentricity

0.00493

Inclination

89.0118°

RAAN

281.5975°

Arg. of periapsis

355.0564°

True anomaly

5.06286°

Mean anomaly

5.0132°

Eccentric anomaly

5.038°

Mean motion

3.55127 °/min

Orbital period

101.37 mins

BSTAR

0.00042855

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

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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.
10 mins	2026-04-28 23:11:51.929Z	0.661° NNE	2026-04-28 23:15:51.929Z	356.811° N	44.218°	2026-04-28 23:21:51.929Z	183.135° SSW
7 mins	2026-04-29 10:35:51.929Z	134.171° SE	2026-04-29 10:38:51.929Z	78.759° E	30.777°	2026-04-29 10:42:51.929Z	19.931° NNE
6 mins	2026-04-29 12:17:51.929Z	241.174° WSW	2026-04-29 12:19:51.929Z	271.396° WNW	22.49°	2026-04-29 12:23:51.929Z	327.368° NNW

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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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View CZ-6A DEB, 61360 on Gunter's Space Page

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CZ-6A DEB, 61360

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: 2026-04-28T10:46:25.555Z)

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, 61360 on other resources

Documentation

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