CZ-4B DEB, 29536

Orbit data source: Space-Track

CZ-4B DEB, 29536 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/29536?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29536, 2006-015C

Orbit

SSO

Last TLE update

17 hours 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 17 hours ago

0 CZ-4B DEB
1 29536U 06015C   25213.84360635  .00010822  00000-0  12145-2 0  9993
2 29536  97.8339 171.1167 0098124 294.2462  64.8524 14.83474108 16414

Epoch: 2025-08-01T20:14Z

TLE epoch observation values (Epoch: 2025-08-01T20:14:47.588Z)

Latitude

-0.00002°

Longitude

-83.26989°

Altitude

592.783 km

Speed

7.579 km/s

True Right ascension

11h 24m 28s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-75.13025°

Longitude

-51.53502°

Altitude

577.807 km

Speed

7.607 km/s

Apparent Right ascension

14h 57m 07s

Apparent Declination

-58° 48' 33"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

03:27:49

Azimuth

168.052° S

Elevation

-70.487°

Doppler factor

Orbital elements

Apogee altitude

684.036 km

Perigee altitude

546.789 km

Semi-major axis

6,993.549 km

Eccentricity

0.00981

Inclination

97.8339°

RAAN

171.1167°

Arg. of periapsis

294.2462°

True anomaly

65.87552°

Mean anomaly

64.8524°

Eccentric anomaly

65.36343°

Mean motion

3.71105 °/min

Orbital period

97.01 mins

BSTAR

0.0012145

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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, 29537

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.
7 mins	2025-08-02 20:39:40.170Z	135.494° SSE	2025-08-02 20:42:40.170Z	83.857° E	31.635°	2025-08-02 20:46:40.170Z	6.073° NNE
4 mins	2025-08-02 22:17:40.170Z	241.04° WSW	2025-08-02 22:19:40.170Z	274.765° WNW	17.155°	2025-08-02 22:21:40.170Z	304.353° NW
7 mins	2025-08-03 10:03:40.170Z	13.929° NNE	2025-08-03 10:06:40.170Z	42.679° NE	44.801°	2025-08-03 10:10:40.170Z	192.169° SSW

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, 29536 on other resources

View CZ-4B DEB, 29536 on Heavens-Above

View CZ-4B DEB, 29536 on Keep Track

View CZ-4B DEB, 29536 on Celestrak

View CZ-4B DEB, 29536 on Gunter's Space Page

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