CZ-4B DEB, 29537

Orbit data source: Space-Track

CZ-4B DEB, 29537 is space debris in SSO originally from a launch on Wed, 26 Apr 2006 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/29537?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29537, 2006-015D

Orbit

SSO

Last TLE update

4 days ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2006-04-26 (19 years 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 4 days ago

0 CZ-4B DEB
1 29537U 06015D   25211.00819622  .00007242  00000-0  10528-2 0  9990
2 29537  97.7927 228.3666 0128223  77.3406 284.2102 14.70692942 14410

Epoch: 2025-07-30T00:11Z

TLE epoch observation values (Epoch: 2025-07-30T00:11:48.153Z)

Latitude

-0.00002°

Longitude

-82.47763°

Altitude

640.807 km

Speed

7.549 km/s

True Right ascension

15h 13m 27s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

42.91934°

Longitude

108.20182°

Altitude

634.309 km

Speed

7.562 km/s

Apparent Right ascension

08h 16m 22s

Apparent Declination

45° 38' 34"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

03:27:49

Azimuth

58.312° ENE

Elevation

38.554°

Doppler factor

Orbital elements

Apogee altitude

746.097 km

Perigee altitude

565.712 km

Semi-major axis

7,034.042 km

Eccentricity

0.01282

Inclination

97.7927°

RAAN

228.3666°

Arg. of periapsis

77.3406°

True anomaly

282.78035°

Mean anomaly

284.2102°

Eccentric anomaly

283.49582°

Mean motion

3.67905 °/min

Orbital period

97.85 mins

BSTAR

0.0010528

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Other satellites on launch #15 in the year 2006 (2006-04-26 UTC)

YAOGAN 1, 29092

CZ-4B R/B, 29093 (Decayed)

CZ-4B DEB, 29536

CZ-4B DEB, 29538

CZ-4B DEB, 29539

YAOGAN 1 DEB, 36363 (Decayed)

YAOGAN 1 DEB, 36364 (Decayed)

YAOGAN 1 DEB, 36365

YAOGAN 1 DEB, 36502 (Decayed)

YAOGAN 1 DEB, 36503 (Decayed)

YAOGAN 1 DEB, 36504 (Decayed)

YAOGAN 1 DEB, 37243 (Decayed)

CZ-4B 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.
5 mins	2025-08-02 13:42:40.398Z	59.004° ENE	2025-08-02 13:43:40.398Z	97.158° ESE	36.21°	2025-08-02 13:47:40.398Z	172.626° S
6 mins	2025-08-03 00:40:40.398Z	129.73° SE	2025-08-03 00:43:40.398Z	56.097° ENE	29.792°	2025-08-03 00:46:40.398Z	6.681° NNE

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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Authenticating...

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Check out CZ-4B DEB, 29537 on other resources

View CZ-4B DEB, 29537 on Heavens-Above

View CZ-4B DEB, 29537 on Keep Track

View CZ-4B DEB, 29537 on Celestrak

View CZ-4B DEB, 29537 on Gunter's Space Page

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