CZ-3A DEB, 35563

Orbit data source: Space-Track

CZ-3A DEB, 35563 is space debris in HEO originally from a launch on Fri, 02 Feb 2007 UTC launched from the Xichang Space Center, China (XSC). 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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https://www.satcat.com/sats-embedded/35563?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

35563, 2007-003X

Orbit

HEO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2007-02-02 (19 years ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.2 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago

0 CZ-3A DEB
1 35563U 07003X   25344.26373767 -.00000227  00000-0  27124-3 0  9992
2 35563  22.2982 221.8589 7440933 354.9330 152.3657  1.89950520 12484

Epoch: 2025-12-10T06:19Z

TLE epoch observation values (Epoch: 2025-12-10T06:19:46.934Z)

Latitude

4.2177°

Longitude

-142.65549°

Altitude

40,857.887 km

Speed

1.551 km/s

True Right ascension

02h 06m 06s

True Declination

4° 12' 50"

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

12:53:10

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

41,662.764 km

Perigee altitude

670.791 km

Semi-major axis

27,544.914 km

Eccentricity

0.74409

Inclination

22.2982°

RAAN

221.8589°

Arg. of periapsis

354.933°

True anomaly

173.86358°

Mean anomaly

152.3657°

Eccentric anomaly

164.06824°

Mean motion

0.47477 °/min

Orbital period

758.27 mins

BSTAR

0.00027124

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Other satellites on launch #3 in the year 2007 (2007-02-02 UTC)

CZ-3A DEB, 35566

CZ-3A DEB, 35553 (Decayed)

CZ-3A R/B, 30324

CZ-3A DEB, 35564

CZ-3A DEB, 39598

CZ-3A DEB, 32381 (Decayed)

CZ-3A DEB, 36970

CZ-3A DEB, 35549

CZ-3A DEB, 35550

CZ-3A DEB, 35560

CZ-3A DEB, 35552

CZ-3A DEB, 35554

CZ-3A DEB, 36966

CZ-3A DEB, 40152

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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

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CZ-3A 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.
352 mins	2025-12-11 02:51:21.137Z	269.389° W	2025-12-11 04:11:21.137Z	241.353° WSW	33.039°	2025-12-11 08:43:21.137Z	256.34° W

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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-3A DEB, 35563 on other resources

View CZ-3A DEB, 35563 on Heavens-Above

View CZ-3A DEB, 35563 on Keep Track

View CZ-3A DEB, 35563 on Celestrak

View CZ-3A DEB, 35563 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

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