CZ-3B DEB, 42472

Orbit data source: Space-Track

CZ-3B DEB, 42472 is space debris in HEO originally from a launch on Mon, 19 Dec 2011 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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Iframe URL

https://www.satcat.com/sats-embedded/42472?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

42472, 2011-077AM

Orbit

HEO

Country

CN / PRC

Related business

China Aerospace Science and Technology Corporation (CASC) (CN)

Manufacturer

CALT

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2011-12-19 (14 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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 6 days ago

TLE from 6 days ago

0 CZ-3B DEB
1 42472U 11077AM  25334.20230973 -.00000041  00000-0  00000-0 0  9994
2 42472  25.9997 350.2527 7186592 185.9483 154.9235  1.79341764 71461

Epoch: 2025-11-30T04:51Z

TLE epoch observation values (Epoch: 2025-11-30T04:51:19.560Z)

Latitude

-0.00006°

Longitude

-151.90248°

Altitude

42,096.832 km

Speed

1.586 km/s

True Right ascension

23h 20m 59s

True Declination

0° 00' 00"

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

15:20:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

42,809.244 km

Perigee altitude

1,673.731 km

Semi-major axis

28,619.624 km

Eccentricity

0.71866

Inclination

25.9997°

RAAN

350.2527°

Arg. of periapsis

185.9483°

True anomaly

174.04251°

Mean anomaly

154.9235°

Eccentric anomaly

165.34263°

Mean motion

0.44828 °/min

Orbital period

803.07 mins

BSTAR

0

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Other satellites on launch #77 in the year 2011 (2011-12-19 UTC)

CZ-3B R/B, 38015 (Decayed)

CZ-3B DEB, 40847

CZ-3B DEB, 40180

CZ-3B DEB, 48546

CZ-3B DEB, 40181

CZ-3B DEB, 40189

CZ-3B DEB, 40185

CZ-3B DEB, 40193

CZ-3B DEB, 40852

CZ-3B DEB, 40850

CZ-3B DEB, 41120

CZ-3B DEB, 40846

CZ-3B DEB, 40843

CZ-3B DEB, 40845

CZ-3B DEB, 40191

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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-3B 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.
219 mins	2025-12-05 21:38:50.070Z	93.096° ESE	2025-12-06 00:07:50.070Z	94.129° ESE	21.942°	2025-12-06 01:17:50.070Z	80.719° E

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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-3B DEB, 42472 on other resources

View CZ-3B DEB, 42472 on Heavens-Above

View CZ-3B DEB, 42472 on Keep Track

View CZ-3B DEB, 42472 on Celestrak

View CZ-3B DEB, 42472 on Gunter's Space Page

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

Documentation

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