CZ-6A DEB, 61419

Orbit data source: Space-Track

CZ-6A DEB, 61419 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/61419?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61419, 2024-140YL

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: 1 day ago

TLE from 1 day ago

0 CZ-6A DEB
1 61419U 24140YL  26054.09741031  .00010266  00000-0  13639-2 0  9993
2 61419  88.9705 280.7290 0106914 248.2447 110.7369 14.75726316 78925

Epoch: 2026-02-23T02:20Z

TLE epoch observation values (Epoch: 2026-02-23T02:20:16.250Z)

Latitude

-0.00003°

Longitude

92.66511°

Altitude

673.261 km

Speed

7.506 km/s

True Right ascension

18h 42m 54s

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

07:22:26

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

714.749 km

Perigee altitude

564.687 km

Semi-major axis

7,017.855 km

Eccentricity

0.01069

Inclination

88.9705°

RAAN

280.729°

Arg. of periapsis

248.2447°

True anomaly

111.8772°

Mean anomaly

110.7369°

Eccentric anomaly

111.3076°

Mean motion

3.69179 °/min

Orbital period

97.51 mins

BSTAR

0.0013639

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

CZ-6A DEB, 61279

CZ-6A DEB, 61495 (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.
6 mins	2026-02-24 14:16:42.145Z	118.754° SE	2026-02-24 14:19:42.145Z	79.645° E	17.406°	2026-02-24 14:22:42.145Z	38.619° NE
8 mins	2026-02-24 15:53:42.145Z	206.923° SW	2026-02-24 15:56:42.145Z	259.937° W	34.619°	2026-02-24 16:01:42.145Z	345.809° N
4 mins	2026-02-25 02:08:42.145Z	56.518° ENE	2026-02-25 02:09:42.145Z	71.409° E	15.734°	2026-02-25 02:12:42.145Z	115.411° SE
7 mins	2026-02-25 03:44:42.145Z	341.637° N	2026-02-25 03:47:42.145Z	289.137° WNW	33.506°	2026-02-25 03:51:42.145Z	209.051° 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, 61419 on other resources

View CZ-6A DEB, 61419 on Heavens-Above

View CZ-6A DEB, 61419 on Keep Track

View CZ-6A DEB, 61419 on Celestrak

View CZ-6A DEB, 61419 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, 61419

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-02-23T02:20:16.250Z)

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, 61419 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago