CZ-6A DEB, 61801

Orbit data source: Space-Track

CZ-6A DEB, 61801 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/61801?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61801, 2024-140ABR

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: 2 days ago

TLE from 2 days ago

0 CZ-6A DEB
1 61801U 24140ABR 26051.96245473  .00004141  00000-0  11418-2 0  9998
2 61801  88.4371 248.0600 0125549  53.8950 307.3798 14.42076185 76991

Epoch: 2026-02-20T23:05Z

TLE epoch observation values (Epoch: 2026-02-20T23:05:56.088Z)

Latitude

-0.00005°

Longitude

110.68443°

Altitude

701.092 km

Speed

7.534 km/s

True Right ascension

16h 32m 14s

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

12:52:41

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

838.045 km

Perigee altitude

659.095 km

Semi-major axis

7,126.707 km

Eccentricity

0.01255

Inclination

88.4371°

RAAN

248.06°

Arg. of periapsis

53.895°

True anomaly

306.22566°

Mean anomaly

307.3798°

Eccentric anomaly

306.80383°

Mean motion

3.60753 °/min

Orbital period

99.79 mins

BSTAR

0.0011418

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

CZ-6A DEB, 61341 (Decayed)

CZ-6A DEB, 60889

CZ-6A DEB, 60756 (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	2026-02-23 12:49:58.312Z	153.375° SSE	2026-02-23 12:53:58.312Z	78.759° E	34.337°	2026-02-23 12:57:58.312Z	14.328° NNE
8 mins	2026-02-24 00:56:58.312Z	6.492° NNE	2026-02-24 01:00:58.312Z	132.001° SE	43.039°	2026-02-24 01:04:58.312Z	174.197° 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, 61801 on other resources

View CZ-6A DEB, 61801 on Heavens-Above

View CZ-6A DEB, 61801 on Keep Track

View CZ-6A DEB, 61801 on Celestrak

View CZ-6A DEB, 61801 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, 61801

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-02-20T23:05:56.088Z)

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, 61801 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago