CZ-6A DEB, 60625

Orbit data source: Space-Track

CZ-6A DEB, 60625 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 src="https://www.satcat.com/sats-embedded/60625?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/60625?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60625, 2024-140AA

Orbit

LEO

Last TLE update

21 hours ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2024-08-06 (11 months ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 21 hours ago

0 CZ-6A DEB
1 60625U 24140AA  25189.85699424  .00002640  00000-0  74591-3 0  9993
2 60625  89.0048 312.1858 0069131  64.5262 296.3072 14.44021333 48290

Epoch: 2025-07-08T20:34Z

TLE epoch observation values (Epoch: 2025-07-08T20:34:04.302Z)

Latitude

0°

Longitude

76.62191°

Altitude

726.776 km

Speed

7.503 km/s

True Right ascension

20h 48m 44s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

-10.66979°

Longitude

-103.29344°

Altitude

781.033 km

Speed

7.447 km/s

Apparent Right ascension

11h 45m 21s

Apparent Declination

-45° 36' 18"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

05:35:02

Azimuth

127.062° SE

Elevation

-28.858°

Doppler factor

Orbital elements

Apogee altitude

791.383 km

Perigee altitude

692.936 km

Semi-major axis

7,120.296 km

Eccentricity

0.00691

Inclination

89.0048°

RAAN

312.1858°

Arg. of periapsis

64.5262°

True anomaly

Unknown

Mean anomaly

296.3072°

Eccentric anomaly

Unknown

Mean motion

3.6124 °/min

Orbital period

99.66 mins

BSTAR

0.00074591

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

QIANFAN-1, 60379

CZ-6A DEB, 61468

CZ-6A DEB, 61469

CZ-6A DEB, 61470 (Decayed)

CZ-6A DEB Visibility forecast

Observer location: undefined°, undefined°

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	2025-07-09 20:24:54.238Z	2.799° NNE	2025-07-09 20:29:54.238Z	156.336° SSE	43.79°	2025-07-09 20:33:54.238Z	179.204° S
5 mins	2025-07-10 07:38:54.238Z	111.876° ESE	2025-07-10 07:40:54.238Z	77.392° E	21.372°	2025-07-10 07:43:54.238Z	32.863° NE
6 mins	2025-07-10 09:17:54.238Z	227.184° WSW	2025-07-10 09:19:54.238Z	264.067° W	27.512°	2025-07-10 09:23:54.238Z	334.059° NNW

Authenticating...

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Check out CZ-6A DEB, 60625 on other resources

View CZ-6A DEB, 60625 on Heavens-Above

View CZ-6A DEB, 60625 on Keep Track

View CZ-6A DEB, 60625 on Celestrak

View CZ-6A DEB, 60625 on Gunter's Space Page

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