CZ-6A DEB, 61827

Orbit data source: Space-Track

CZ-6A DEB, 61827 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/61827?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61827, 2024-140ACT

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: 6 hours ago

TLE from 6 hours ago

0 CZ-6A DEB
1 61827U 24140ACT 26114.85336307  .00001926  00000-0  10193-2 0  9998
2 61827  88.8540 271.8366 0104232  45.1629 315.7965 14.10600417 83125

Epoch: 2026-04-24T20:28Z

TLE epoch observation values (Epoch: 2026-04-24T20:28:50.569Z)

Latitude

-0.0001°

Longitude

111.74577°

Altitude

806.668 km

Speed

7.478 km/s

True Right ascension

18h 07m 20s

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

09:43:16

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

929.668 km

Perigee altitude

778.898 km

Semi-major axis

7,232.42 km

Eccentricity

0.01042

Inclination

88.854°

RAAN

271.8366°

Arg. of periapsis

45.1629°

True anomaly

314.95593°

Mean anomaly

315.7965°

Eccentric anomaly

315.377°

Mean motion

3.52872 °/min

Orbital period

102.02 mins

BSTAR

0.0010193

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

QIANFAN-12, 60390

QIANFAN-16, 60394

CZ-6A DEB, 61433 (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	2026-04-25 10:13:14.156Z	144.148° SSE	2026-04-25 10:17:14.156Z	83.306° E	30.865°	2026-04-25 10:21:14.156Z	20.458° NNE
6 mins	2026-04-25 11:57:14.156Z	244.08° WSW	2026-04-25 11:59:14.156Z	274.678° WNW	21.442°	2026-04-25 12:03:14.156Z	328.593° NNW
9 mins	2026-04-25 22:36:14.156Z	5.427° NNE	2026-04-25 22:40:14.156Z	93.789° ESE	44.396°	2026-04-25 22:45:14.156Z	176.706° 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, 61827 on other resources

View CZ-6A DEB, 61827 on Heavens-Above

View CZ-6A DEB, 61827 on Keep Track

View CZ-6A DEB, 61827 on Celestrak

View CZ-6A DEB, 61827 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, 61827

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 6 hours ago

TLE from 6 hours ago

TLE epoch observation values (Epoch: 2026-04-24T20:28:50.569Z)

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, 61827 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 6 hours ago