CZ-4B DEB, 29538

Orbit data source: Space-Track

CZ-4B DEB, 29538 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/29538?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29538, 2006-015E

Orbit

SSO

Last TLE update

1 day 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 1 day ago

0 CZ-4B DEB
1 29538U 06015E   25213.26929611  .00023700  00000-0  17270-2 0  9999
2 29538  98.0468 330.1140 0068554  89.7025 271.2053 15.01837486 20617

Epoch: 2025-08-01T06:27Z

TLE epoch observation values (Epoch: 2025-08-01T06:27:47.183Z)

Latitude

-0.00012°

Longitude

-76.95482°

Altitude

563.603 km

Speed

7.58 km/s

True Right ascension

22h 00m 27s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

-45.80093°

Longitude

96.08685°

Altitude

615.477 km

Speed

7.53 km/s

Apparent Right ascension

12h 34m 31s

Apparent Declination

-52° 49' 57"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

03:35:42

Azimuth

128.249° SE

Elevation

-56.856°

Doppler factor

Orbital elements

Apogee altitude

605.8 km

Perigee altitude

510.697 km

Semi-major axis

6,936.386 km

Eccentricity

0.00686

Inclination

98.0468°

RAAN

330.114°

Arg. of periapsis

89.7025°

True anomaly

270.41979°

Mean anomaly

271.2053°

Eccentric anomaly

270.81255°

Mean motion

3.75702 °/min

Orbital period

95.82 mins

BSTAR

0.001727

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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, 29537

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.
4 mins	2025-08-02 19:49:31.874Z	57.204° ENE	2025-08-02 19:51:31.874Z	92.424° ESE	17.039°	2025-08-02 19:53:31.874Z	128.958° SE
5 mins	2025-08-02 21:24:31.874Z	336.868° NNW	2025-08-02 21:26:31.874Z	290.741° WNW	25.769°	2025-08-02 21:29:31.874Z	232.032° WSW
5 mins	2025-08-03 08:10:31.874Z	196.016° SSW	2025-08-03 08:12:31.874Z	270.323° WNW	37.413°	2025-08-03 08:15:31.874Z	334.184° NNW

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, 29538 on other resources

View CZ-4B DEB, 29538 on Heavens-Above

View CZ-4B DEB, 29538 on Keep Track

View CZ-4B DEB, 29538 on Celestrak

View CZ-4B DEB, 29538 on Gunter's Space Page

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