CZ-4C R/B, 40276

Orbit data source: Space-Track

CZ-4C R/B, 40276 is space debris in SSO originally from a launch on Mon, 20 Oct 2014 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/40276?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40276, 2014-063B

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

CZ-4 STAGE 3, Unknown motor

Mass

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

Launch date (UTC)

2014-10-20 (12 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 2.9 m

Radar Cross Section

14.536 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 CZ-4C R/B
1 40276U 14063B   26297.24386777 -.00000039  00000-0  14408-4 0  9997
2 40276 100.2372 225.0816 0142204 303.5731  55.1888 13.43041760588831

Epoch: 2026-10-24T05:51Z

TLE epoch observation values (Epoch: 2026-10-24T05:51:10.175Z)

Latitude

-0.00004°

Longitude

104.63636°

Altitude

1,041.057 km

Speed

7.361 km/s

True Right ascension

15h 00m 19s

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

00:40:22

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,201.583 km

Perigee altitude

989.033 km

Semi-major axis

7,473.445 km

Eccentricity

0.01422

Inclination

100.2372°

RAAN

225.0816°

Arg. of periapsis

303.5731°

True anomaly

56.5403°

Mean anomaly

55.1888°

Eccentric anomaly

55.86318°

Mean motion

3.3594 °/min

Orbital period

107.16 mins

BSTAR

0.000014408

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Other satellites on launch #63 in the year 2014 (2014-10-20 UTC)

YAOGAN 22, 40275

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CZ-4C R/B 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.
12 mins	2026-10-25 07:29:21.529Z	30.953° NE	2026-10-25 07:35:21.529Z	92.218° ESE	41.7°	2026-10-25 07:41:21.529Z	164.186° S
11 mins	2026-10-25 09:16:21.529Z	352.929° N	2026-10-25 09:21:21.529Z	291.488° WNW	38.654°	2026-10-25 09:27:21.529Z	231.803° WSW
8 mins	2026-10-25 17:47:21.529Z	95.148° ESE	2026-10-25 17:50:21.529Z	62.031° ENE	23.592°	2026-10-25 17:55:21.529Z	12.154° NNE
12 mins	2026-10-25 19:30:21.529Z	177.311° S	2026-10-25 19:35:21.529Z	244.492° WSW	65.668°	2026-10-25 19:42:21.529Z	338.959° N

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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-4C R/B, 40276 on other resources

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View CZ-4C R/B, 40276 on Keep Track

View CZ-4C R/B, 40276 on Celestrak

View CZ-4C R/B, 40276 on Gunter's Space Page

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CZ-4C R/B, 40276

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-10-24T05:51:10.175Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #63 in the year 2014 (2014-10-20 UTC)

CZ-4C R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4C R/B, 40276 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago