CZ-6A DEB, 61395

Orbit data source: Space-Track

CZ-6A DEB, 61395 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/61395?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61395, 2024-140XL

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: 11 hours ago

TLE from 11 hours ago

0 CZ-6A DEB
1 61395U 24140XL  26113.70509162  .00000262  00000-0  12027-3 0  9993
2 61395  88.9596 278.5086 0055779 353.7087   6.3394 14.17685886 84318

Epoch: 2026-04-23T16:55Z

TLE epoch observation values (Epoch: 2026-04-23T16:55:19.915Z)

Latitude

-0.00009°

Longitude

172.92728°

Altitude

796.255 km

Speed

7.476 km/s

True Right ascension

18h 34m 02s

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

11:10:26

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

870.351 km

Perigee altitude

789.937 km

Semi-major axis

7,208.281 km

Eccentricity

0.00558

Inclination

88.9596°

RAAN

278.5086°

Arg. of periapsis

353.7087°

True anomaly

6.41047°

Mean anomaly

6.3394°

Eccentric anomaly

6.37489°

Mean motion

3.54646 °/min

Orbital period

101.51 mins

BSTAR

0.00012027

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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 10:01:05.860Z	103.124° ESE	2026-04-24 10:03:05.860Z	79.858° E	14.238°	2026-04-24 10:06:05.860Z	44.253° NE
8 mins	2026-04-24 11:41:05.860Z	195.389° SSW	2026-04-24 11:44:05.860Z	248.639° W	41.167°	2026-04-24 11:49:05.860Z	350.936° N
8 mins	2026-04-24 22:19:05.860Z	33.843° NE	2026-04-24 22:22:05.860Z	75.518° E	25.583°	2026-04-24 22:27:05.860Z	140.538° SSE
8 mins	2026-04-25 00:00:05.860Z	336.842° NNW	2026-04-25 00:04:05.860Z	277.58° WNW	30.061°	2026-04-25 00:08:05.860Z	220.519° 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, 61395 on other resources

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View CZ-6A DEB, 61395 on Celestrak

View CZ-6A DEB, 61395 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, 61395

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-04-23T16:55:19.915Z)

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, 61395 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago