CZ-6A DEB, 60708

Orbit data source: Space-Track

CZ-6A DEB, 60708 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/60708?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60708, 2024-140DM

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: 13 hours ago

TLE from 13 hours ago

0 CZ-6A DEB
1 60708U 24140DM  26118.44616275  .00001830  00000-0  69593-3 0  9992
2 60708  88.9998 279.6121 0041995  32.5633 327.8139 14.30127388 89111

Epoch: 2026-04-28T10:42Z

TLE epoch observation values (Epoch: 2026-04-28T10:42:28.461Z)

Latitude

-0.00009°

Longitude

-97.42785°

Altitude

768.922 km

Speed

7.483 km/s

True Right ascension

18h 38m 26s

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

07:30:22

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

818.337 km

Perigee altitude

758.146 km

Semi-major axis

7,166.379 km

Eccentricity

0.0042

Inclination

88.9998°

RAAN

279.6121°

Arg. of periapsis

32.5633°

True anomaly

327.55642°

Mean anomaly

327.8139°

Eccentric anomaly

327.68528°

Mean motion

3.57761 °/min

Orbital period

100.63 mins

BSTAR

0.00069593

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

CZ-6A DEB, 61392 (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	2026-04-29 10:19:58.116Z	140.529° SSE	2026-04-29 10:23:58.116Z	88.731° E	26.687°	2026-04-29 10:27:58.116Z	25.407° NE
7 mins	2026-04-29 12:01:58.116Z	229.256° WSW	2026-04-29 12:04:58.116Z	276.898° WNW	24.725°	2026-04-29 12:08:58.116Z	332.942° NNW
8 mins	2026-04-29 22:33:58.116Z	19.634° NNE	2026-04-29 22:36:58.116Z	74.653° E	37.623°	2026-04-29 22:41:58.116Z	162.03° 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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View CZ-6A DEB, 60708 on Gunter's Space Page

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CZ-6A DEB, 60708

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 13 hours ago

TLE from 13 hours ago

TLE epoch observation values (Epoch: 2026-04-28T10:42:28.461Z)

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, 60708 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 13 hours ago