CZ-6A DEB, 60686

Orbit data source: Space-Track

CZ-6A DEB, 60686 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/60686?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60686, 2024-140CP

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: 9 hours ago

TLE from 9 hours ago

0 CZ-6A DEB
1 60686U 24140CP  26130.13555951  .00001087  00000-0  32668-3 0  9997
2 60686  88.9800 275.3162 0050429  14.6315 345.6333 14.41312221 91904

Epoch: 2026-05-10T03:15Z

TLE epoch observation values (Epoch: 2026-05-10T03:15:12.341Z)

Latitude

0.00001°

Longitude

-1.4282°

Altitude

722.411 km

Speed

7.512 km/s

True Right ascension

18h 21m 15s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

20:39:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

787.039 km

Perigee altitude

715.135 km

Semi-major axis

7,129.224 km

Eccentricity

0.00504

Inclination

88.98°

RAAN

275.3162°

Arg. of periapsis

14.6315°

True anomaly

345.48903°

Mean anomaly

345.6333°

Eccentric anomaly

345.56126°

Mean motion

3.60562 °/min

Orbital period

99.84 mins

BSTAR

0.00032668

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

CZ-6A DEB, 61344 (Decayed)

CZ-6A DEB, 61140 (Decayed)

CZ-6A DEB, 61156 (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	2026-05-10 22:10:29.375Z	352.727° N	2026-05-10 22:13:29.375Z	283.513° WNW	43.504°	2026-05-10 22:18:29.375Z	190.494° SSW
6 mins	2026-05-11 09:23:29.375Z	128.651° SE	2026-05-11 09:25:29.375Z	91.125° ESE	28.5°	2026-05-11 09:29:29.375Z	22.894° NE
6 mins	2026-05-11 11:03:29.375Z	240.156° WSW	2026-05-11 11:05:29.375Z	271.874° WNW	21.474°	2026-05-11 11:09:29.375Z	329.119° 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, 60686 on other resources

View CZ-6A DEB, 60686 on Heavens-Above

View CZ-6A DEB, 60686 on Keep Track

View CZ-6A DEB, 60686 on Celestrak

View CZ-6A DEB, 60686 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, 60686

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2026-05-10T03:15:12.341Z)

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, 60686 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 9 hours ago