CZ-6A DEB, 61102

Orbit data source: Space-Track

CZ-6A DEB, 61102 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/61102?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61102, 2024-140NU

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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago

0 CZ-6A DEB
1 61102U 24140NU  26171.16695957  .00010933  00000-0  99255-3 0  9995
2 61102  88.7295 243.0023 0128913 113.9179 247.5616 14.88965301 97697

Epoch: 2026-06-20T04:00Z

TLE epoch observation values (Epoch: 2026-06-20T04:00:25.306Z)

Latitude

-0.00001°

Longitude

-85.48862°

Altitude

639.652 km

Speed

7.519 km/s

True Right ascension

16h 12m 00s

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

07:22:56

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

687.953 km

Perigee altitude

508.089 km

Semi-major axis

6,976.158 km

Eccentricity

0.01289

Inclination

88.7295°

RAAN

243.0023°

Arg. of periapsis

113.9179°

True anomaly

246.20468°

Mean anomaly

247.5616°

Eccentric anomaly

246.88229°

Mean motion

3.72493 °/min

Orbital period

96.65 mins

BSTAR

0.00099255

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

CZ-6A DEB, 60882

CZ-6A DEB, 61384 (Decayed)

CZ-6A DEB, 60744 (Decayed)

CZ-6A DEB, 60849

CZ-6A DEB, 60885

CZ-6A DEB, 61344 (Decayed)

CZ-6A DEB, 60711

CZ-6A DEB, 60799

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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	2026-06-21 04:20:09.784Z	125.613° SE	2026-06-21 04:23:09.784Z	77.598° E	18.309°	2026-06-21 04:25:09.784Z	42.853° NE
5 mins	2026-06-21 05:57:09.784Z	225.485° WSW	2026-06-21 05:59:09.784Z	263.018° W	24.562°	2026-06-21 06:02:09.784Z	326.354° NNW
5 mins	2026-06-21 17:41:09.784Z	325.353° NNW	2026-06-21 17:43:09.784Z	277.671° WNW	26.581°	2026-06-21 17:46:09.784Z	218.109° 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, 61102 on other resources

View CZ-6A DEB, 61102 on Heavens-Above

View CZ-6A DEB, 61102 on Keep Track

View CZ-6A DEB, 61102 on Celestrak

View CZ-6A DEB, 61102 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, 61102

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2026-06-20T04:00:25.306Z)

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, 61102 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 16 hours ago