CZ-2C R/B, 40262

Orbit data source: Space-Track

CZ-2C R/B, 40262 is space debris in SSO originally from a launch on Sun, 28 Sep 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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https://www.satcat.com/sats-embedded/40262?theme=dark&initialShowStats=false

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Identifier

40262, 2014-059B

Orbit

SSO

Country

CN / PRC

Related business

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

Manufacturer

CALT

Mission

Spacecraft

Bus & Motor

CZ-2 STAGE 2, Unknown motor

Mass

~3,800 kg wet, ~3,800 kg dry

Launch date (UTC)

2014-09-28 (12 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 4.1 m

Radar Cross Section

23.715 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 CZ-2C R/B
1 40262U 14059B   26296.16545293  .00000555  00000-0  86390-4 0  9998
2 40262  98.3384 162.0177 0042095 135.5802 224.8796 14.76599730648501

Epoch: 2026-10-23T03:58Z

TLE epoch observation values (Epoch: 2026-10-23T03:58:15.133Z)

Latitude

0.00003°

Longitude

70.86473°

Altitude

664.081 km

Speed

7.514 km/s

True Right ascension

10h 48m 04s

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

13:17:16

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

666.674 km

Perigee altitude

607.612 km

Semi-major axis

7,015.28 km

Eccentricity

0.00421

Inclination

98.3384°

RAAN

162.0177°

Arg. of periapsis

135.5802°

True anomaly

224.54049°

Mean anomaly

224.8796°

Eccentric anomaly

224.70992°

Mean motion

3.69382 °/min

Orbital period

97.46 mins

BSTAR

0.00008639

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Other satellites on launch #59 in the year 2014 (2014-09-28 UTC)

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CZ-2C 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.
7 mins	2026-10-24 03:19:03.732Z	40.373° NE	2026-10-24 03:22:03.732Z	85.606° E	24.959°	2026-10-24 03:26:03.732Z	152.821° SSE
5 mins	2026-10-24 04:57:03.732Z	329.332° NNW	2026-10-24 04:59:03.732Z	287.842° WNW	25.794°	2026-10-24 05:02:03.732Z	238.607° WSW
5 mins	2026-10-24 14:17:03.732Z	106.281° ESE	2026-10-24 14:19:03.732Z	71.552° E	23.132°	2026-10-24 14:22:03.732Z	21.4° NNE
6 mins	2026-10-24 15:53:03.732Z	212.22° SW	2026-10-24 15:55:03.732Z	249.392° W	30.464°	2026-10-24 15:59:03.732Z	322.738° NNW

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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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CZ-2C R/B, 40262

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-10-23T03:58:15.133Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #59 in the year 2014 (2014-09-28 UTC)

CZ-2C R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-2C R/B, 40262 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago