CZ-2C R/B, 43084

Orbit data source: Space-Track

CZ-2C R/B, 43084 is space debris in LEO originally from a launch on Mon, 25 Dec 2017 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/43084?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

43084, 2017-085D

Orbit

LEO

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)

2017-12-25 (8 years ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 3.7 m

Radar Cross Section

23.715 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago

0 CZ-2C R/B
1 43084U 17085D   26171.41246919  .00009872  00000-0  23901-3 0  9997
2 43084  34.6575 217.1968 0050285  88.9396 271.7078 15.38906009469145

Epoch: 2026-06-20T09:53Z

TLE epoch observation values (Epoch: 2026-06-20T09:53:57.338Z)

Latitude

-0.00001°

Longitude

160.08042°

Altitude

447.356 km

Speed

7.647 km/s

True Right ascension

14h 28m 47s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

21:28:25

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

487.019 km

Perigee altitude

418.322 km

Semi-major axis

6,830.807 km

Eccentricity

0.00503

Inclination

34.6575°

RAAN

217.1968°

Arg. of periapsis

88.9396°

True anomaly

271.13173°

Mean anomaly

271.7078°

Eccentric anomaly

271.41978°

Mean motion

3.84446 °/min

Orbital period

93.64 mins

BSTAR

0.00023901

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Other satellites on launch #85 in the year 2017 (2017-12-25 UTC)

YAOGAN-30 J DEB, 45485 (Decayed)

YAOGAN-30 G, 43081

YAOGAN-30 J, 43083

YAOGAN-30 H, 43082

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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.
4 mins	2026-06-23 06:41:24.490Z	210.388° SW	2026-06-23 06:43:24.490Z	160.132° S	22.193°	2026-06-23 06:45:24.490Z	117.329° SE
4 mins	2026-06-23 08:20:24.490Z	219.929° SW	2026-06-23 08:21:24.490Z	186.221° SSW	27.837°	2026-06-23 08:24:24.490Z	118.311° SE

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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-2C R/B, 43084 on other resources

View CZ-2C R/B, 43084 on Heavens-Above

View CZ-2C R/B, 43084 on Keep Track

View CZ-2C R/B, 43084 on Celestrak

View CZ-2C R/B, 43084 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-2C R/B, 43084

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-06-20T09:53:57.338Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #85 in the year 2017 (2017-12-25 UTC)

CZ-2C R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-2C R/B, 43084 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago