CZ-6A DEB, 61308

Orbit data source: Space-Track

CZ-6A DEB, 61308 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/61308?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61308, 2024-140TV

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: 14 hours ago

TLE from 14 hours ago

0 CZ-6A DEB
1 61308U 24140TV  26171.28111531  .00001818  00000-0  31537-3 0  9998
2 61308  88.8991 260.3255 0127000 230.7623 128.2266 14.62616262 96489

Epoch: 2026-06-20T06:44Z

TLE epoch observation values (Epoch: 2026-06-20T06:44:48.362Z)

Latitude

-0.00001°

Longitude

-109.374°

Altitude

744.062 km

Speed

7.453 km/s

True Right ascension

17h 21m 18s

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

07:22:40

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

771.288 km

Perigee altitude

591.97 km

Semi-major axis

7,059.766 km

Eccentricity

0.0127

Inclination

88.8991°

RAAN

260.3255°

Arg. of periapsis

230.7623°

True anomaly

129.35865°

Mean anomaly

128.2266°

Eccentric anomaly

128.79374°

Mean motion

3.65896 °/min

Orbital period

98.39 mins

BSTAR

0.00031537

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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.
9 mins	2026-06-21 05:50:54.095Z	152.155° SSE	2026-06-21 05:54:54.095Z	97.758° ESE	34.27°	2026-06-21 05:59:54.095Z	14.006° NNE
5 mins	2026-06-21 07:31:54.095Z	248.745° W	2026-06-21 07:33:54.095Z	278.005° WNW	19.447°	2026-06-21 07:36:54.095Z	319.183° NNW
7 mins	2026-06-21 17:49:54.095Z	21.96° NNE	2026-06-21 17:52:54.095Z	96.658° ESE	36.482°	2026-06-21 17:56:54.095Z	161.421° 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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Check out CZ-6A DEB, 61308 on other resources

View CZ-6A DEB, 61308 on Heavens-Above

View CZ-6A DEB, 61308 on Keep Track

View CZ-6A DEB, 61308 on Celestrak

View CZ-6A DEB, 61308 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, 61308

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-06-20T06:44:48.362Z)

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, 61308 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago