CZ-4C R/B, 40112

Orbit data source: Space-Track

CZ-4C R/B, 40112 is space debris in LEO originally from a launch on Sat, 09 Aug 2014 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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 src="https://www.satcat.com/sats-embedded/40112?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/40112?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40112, 2014-047D

Orbit

LEO

Last TLE update

16 hours ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

CZ-4 STAGE 3, Unknown motor

Mass

~1,000 kg wet, ~1,000 kg dry

Launch date (UTC)

2014-08-09 (11 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 1.4 m

Radar Cross Section

20.385 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 16 hours ago

0 CZ-4C R/B
1 40112U 14047D   25199.67797922  .00000033  00000-0  61708-4 0  9991
2 40112  63.4154  81.9076 0528394 359.7381   0.3305 13.70168684547103

Epoch: 2025-07-18T16:16Z

TLE epoch observation values (Epoch: 2025-07-18T16:16:17.404Z)

Latitude

-0.00004°

Longitude

-98.89093°

Altitude

610.931 km

Speed

7.751 km/s

True Right ascension

05h 27m 37s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

53.85784°

Longitude

36.30117°

Altitude

1,159.822 km

Speed

7.203 km/s

Apparent Right ascension

11h 47m 20s

Apparent Declination

15° 08' 54"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:23:23

Azimuth

321.044° NNW

Elevation

-25.553°

Doppler factor

Orbital elements

Apogee altitude

1,387.512 km

Perigee altitude

608.035 km

Semi-major axis

7,375.911 km

Eccentricity

0.05284

Inclination

63.4154°

RAAN

81.9076°

Arg. of periapsis

359.7381°

True anomaly

0.36789°

Mean anomaly

0.3305°

Eccentric anomaly

0.34894°

Mean motion

3.42626 °/min

Orbital period

105.07 mins

BSTAR

0.000061708

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Other satellites on launch #47 in the year 2014 (2014-08-09 UTC)

CZ-4C DEB, 49945 (Decayed)

CZ-4C DEB, 49946 (Decayed)

CZ-4C R/B 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.
6 mins	2025-07-19 16:55:16.536Z	156.57° SSE	2025-07-19 16:58:16.536Z	110.325° ESE	21.052°	2025-07-19 17:01:16.536Z	66.896° ENE
8 mins	2025-07-19 18:43:16.536Z	250.947° W	2025-07-19 18:46:16.536Z	313.365° NW	33.646°	2025-07-19 18:51:16.536Z	22.455° NNE
7 mins	2025-07-20 00:17:16.536Z	6.095° NNE	2025-07-20 00:20:16.536Z	35.839° NE	17.446°	2025-07-20 00:24:16.536Z	69.651° E
13 mins	2025-07-20 02:04:16.536Z	335.562° NNW	2025-07-20 02:10:16.536Z	66.64° ENE	41.35°	2025-07-20 02:17:16.536Z	131.594° SE
12 mins	2025-07-20 03:53:16.536Z	299.275° NW	2025-07-20 03:58:16.536Z	247.964° W	28.343°	2025-07-20 04:05:16.536Z	189.675° 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-4C R/B, 40112 on other resources

View CZ-4C R/B, 40112 on Heavens-Above

View CZ-4C R/B, 40112 on Keep Track

View CZ-4C R/B, 40112 on Celestrak

View CZ-4C R/B, 40112 on Gunter's Space Page

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