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

18 hours ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2024-08-06 (9 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 18 hours ago

0 CZ-6A DEB
1 60625U 24140AA  25122.90264191  .00008776  00000-0  25312-2 0  9997
2 60625  89.0049 320.0545 0065737 288.7002  70.7073 14.43335814 38635

Epoch: 2025-05-02T21:39Z

Definitive object data (Epoch: 2025-05-02T21:39:48.261Z)

Latitude

-0.00003°

Longitude

134.05083°

Altitude

735.38 km

Speed

7.495 km/s

True Right ascension

21h 20m 13s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-71.94019°

Longitude

130.92592°

Altitude

727.364 km

Speed

7.515 km/s

Apparent Right ascension

12h 53m 04s

Apparent Declination

-72° 56' 10"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

23:24:53

Azimuth

191.151° SSW

Elevation

-55.289°

Doppler factor

Orbital elements

Apogee altitude

791.237 km

Perigee altitude

697.594 km

Semi-major axis

7,122.553 km

Eccentricity

0.0065737

Inclination

89.0049°

RAAN

320.0545°

Arg. of periapsis

288.7002°

True anomaly

71.4202°

Mean anomaly

70.7073°

Eccentric anomaly

71.06356°

Mean motion

3.61069 °/min

BSTAR

0.0025312

Orbital period

99.7 mins

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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.
8 mins	2025-05-04 00:52:12.568Z	18.627° NNE	2025-05-04 00:56:12.568Z	85.663° E	34.959°	2025-05-04 01:00:12.568Z	154.313° SSE
6 mins	2025-05-04 02:33:12.568Z	316.805° NNW	2025-05-04 02:35:12.568Z	289.522° WNW	19.244°	2025-05-04 02:39:12.568Z	237.778° WSW
8 mins	2025-05-04 13:43:12.568Z	191.817° SSW	2025-05-04 13:47:12.568Z	296.795° NW	41.751°	2025-05-04 13:51:12.568Z	351.541° N

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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