CZ-6A DEB, 60895

Orbit data source: Space-Track

CZ-6A DEB, 60895 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/60895?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60895, 2024-140LA

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: 10 hours ago

TLE from 10 hours ago

0 CZ-6A DEB
1 60895U 24140LA  26114.25024755  .00001667  00000-0  74034-3 0  9994
2 60895  89.3518 306.8298 0051168   6.0297 354.1499 14.21932843 87079

Epoch: 2026-04-24T06:00Z

TLE epoch observation values (Epoch: 2026-04-24T06:00:21.388Z)

Latitude

0.00001°

Longitude

4.45502°

Altitude

785.241 km

Speed

7.48 km/s

True Right ascension

20h 27m 19s

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

23:05:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

852.58 km

Perigee altitude

778.96 km

Semi-major axis

7,193.907 km

Eccentricity

0.00512

Inclination

89.3518°

RAAN

306.8298°

Arg. of periapsis

6.0297°

True anomaly

354.08975°

Mean anomaly

354.1499°

Eccentric anomaly

354.11987°

Mean motion

3.5571 °/min

Orbital period

101.21 mins

BSTAR

0.00074034

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

CZ-6A DEB, 61798

CZ-6A DEB, 61353 (Decayed)

CZ-6A DEB, 60629 (Decayed)

CZ-6A DEB, 61392 (Decayed)

CZ-6A DEB, 60851 (Decayed)

CZ-6A DEB, 61795 (Decayed)

CZ-6A DEB, 61433 (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.
9 mins	2026-04-25 01:09:59.649Z	0.846° NNE	2026-04-25 01:13:59.649Z	350.429° N	44.602°	2026-04-25 01:18:59.649Z	183.929° SSW
8 mins	2026-04-25 12:31:59.649Z	141.472° SSE	2026-04-25 12:35:59.649Z	72.753° E	31.086°	2026-04-25 12:39:59.649Z	17.601° NNE
7 mins	2026-04-25 14:13:59.649Z	234.963° WSW	2026-04-25 14:16:59.649Z	278.261° WNW	21.79°	2026-04-25 14:20:59.649Z	329.724° 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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Check out CZ-6A DEB, 60895 on other resources

View CZ-6A DEB, 60895 on Heavens-Above

View CZ-6A DEB, 60895 on Keep Track

View CZ-6A DEB, 60895 on Celestrak

View CZ-6A DEB, 60895 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, 60895

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-04-24T06:00:21.388Z)

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, 60895 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago