CZ-4B DEB, 29539

Orbit data source: Space-Track

CZ-4B DEB, 29539 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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https://www.satcat.com/sats-embedded/29539?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29539, 2006-015F

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2006-04-26 (20 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago

0 CZ-4B DEB
1 29539U 06015F   26071.64929976  .00014703  00000-0  11367-2 0  9993
2 29539  97.7668 140.9461 0069379  23.7201 131.6418 14.99679811 55107

Epoch: 2026-03-12T15:34Z

TLE epoch observation values (Epoch: 2026-03-12T15:34:59.499Z)

Latitude

23.83693°

Longitude

-79.66195°

Altitude

603.102 km

Speed

7.543 km/s

True Right ascension

21h 37m 31s

True Declination

23° 42' 26"

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

01:01:19

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

613.063 km

Perigee altitude

516.723 km

Semi-major axis

6,943.03 km

Eccentricity

0.00694

Inclination

97.7668°

RAAN

140.9461°

Arg. of periapsis

23.7201°

True anomaly

132.23252°

Mean anomaly

131.6418°

Eccentric anomaly

131.9375°

Mean motion

3.75163 °/min

Orbital period

95.96 mins

BSTAR

0.0011367

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

YAOGAN 1, 29092

CZ-4B DEB, 29538

YAOGAN 1 DEB, 36503 (Decayed)

YAOGAN 1 DEB, 36364 (Decayed)

YAOGAN 1 DEB, 36504 (Decayed)

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

YAOGAN 1 DEB, 36363 (Decayed)

CZ-4B DEB, 29536

YAOGAN 1 DEB, 36365

CZ-4B DEB, 29537

YAOGAN 1 DEB, 36502 (Decayed)

YAOGAN 1 DEB, 37243 (Decayed)

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CZ-4B 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.
5 mins	2026-03-13 03:50:46.913Z	122.214° SE	2026-03-13 03:53:46.913Z	62.18° ENE	22.77°	2026-03-13 03:55:46.913Z	22.611° NE
6 mins	2026-03-13 17:05:46.913Z	33.982° NE	2026-03-13 17:07:46.913Z	83.401° E	36.792°	2026-03-13 17:11:46.913Z	174.299° S

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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-4B DEB, 29539 on other resources

View CZ-4B DEB, 29539 on Heavens-Above

View CZ-4B DEB, 29539 on Keep Track

View CZ-4B DEB, 29539 on Celestrak

View CZ-4B DEB, 29539 on Gunter's Space Page

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

CZ-4B DEB, 29539

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 5 hours ago

TLE from 5 hours ago

TLE epoch observation values (Epoch: 2026-03-12T15:34:59.499Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

CZ-4B DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4B DEB, 29539 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 5 hours ago