CZ-6A DEB, 60814

Orbit data source: Space-Track

CZ-6A DEB, 60814 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/60814?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60814, 2024-140GR

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, 0.2 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 60814U 24140GR  26113.93816956  .00000637  00000-0  33660-3 0  9997
2 60814  89.0594 286.6076 0090440  35.0856 325.6240 14.10600655 87279

Epoch: 2026-04-23T22:30Z

TLE epoch observation values (Epoch: 2026-04-23T22:30:57.849Z)

Latitude

-0.00003°

Longitude

96.88849°

Altitude

806.528 km

Speed

7.478 km/s

True Right ascension

19h 06m 25s

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

15:59:25

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

919.691 km

Perigee altitude

788.871 km

Semi-major axis

7,232.418 km

Eccentricity

0.00904

Inclination

89.0594°

RAAN

286.6076°

Arg. of periapsis

35.0856°

True anomaly

325.03335°

Mean anomaly

325.624°

Eccentric anomaly

325.32923°

Mean motion

3.52873 °/min

Orbital period

102.02 mins

BSTAR

0.0003366

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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.
5 mins	2026-04-24 10:35:17.609Z	104.48° ESE	2026-04-24 10:37:17.609Z	80.752° E	14.557°	2026-04-24 10:40:17.609Z	44.079° NE
9 mins	2026-04-24 12:15:17.609Z	195.333° SSW	2026-04-24 12:19:17.609Z	274.228° WNW	40.54°	2026-04-24 12:24:17.609Z	350.842° N
9 mins	2026-04-24 22:56:17.609Z	28.008° NE	2026-04-24 23:00:17.609Z	85.606° E	27.958°	2026-04-24 23:05:17.609Z	146.357° SSE
7 mins	2026-04-25 00:39:17.609Z	326.175° NNW	2026-04-25 00:42:17.609Z	277.465° WNW	27.928°	2026-04-25 00:46:17.609Z	223.98° SW

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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, 60814 on other resources

View CZ-6A DEB, 60814 on Heavens-Above

View CZ-6A DEB, 60814 on Keep Track

View CZ-6A DEB, 60814 on Celestrak

View CZ-6A DEB, 60814 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, 60814

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: 2026-04-23T22:30:57.849Z)

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, 60814 on other resources

Documentation

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