CZ-6A R/B, 60214

Orbit data source: Space-Track

CZ-6A R/B, 60214 is space debris in SSO originally from a launch on Thu, 04 Jul 2024 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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Iframe URL

https://www.satcat.com/sats-embedded/60214?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60214, 2024-126D

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

CZ-6A STAGE 2, YF-115

Mass

~6,000 kg wet, ~6,000 kg dry

Launch date (UTC)

2024-07-04 (1 year ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 5.5 m

Radar Cross Section

Large (>1 m²)

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Last TLE update: 15 hours ago

TLE from 15 hours ago

0 CZ-6A R/B
1 60214U 24126D   25353.51164669  .00003212  00000-0  17813-3 0  9995
2 60214  97.7947  15.5992 0070557  16.7658 343.5880 15.12418857 80265

Epoch: 2025-12-19T12:16Z

TLE epoch observation values (Epoch: 2025-12-19T12:16:46.274Z)

Latitude

-0.00006°

Longitude

103.05465°

Altitude

485.164 km

Speed

7.648 km/s

True Right ascension

01h 02m 23s

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

02:35:35

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

574.531 km

Perigee altitude

477.106 km

Semi-major axis

6,903.956 km

Eccentricity

0.00706

Inclination

97.7947°

RAAN

15.5992°

Arg. of periapsis

16.7658°

True anomaly

343.35761°

Mean anomaly

343.588°

Eccentric anomaly

343.473°

Mean motion

3.78352 °/min

Orbital period

95.15 mins

BSTAR

0.00017813

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Other satellites on launch #126 in the year 2024 (2024-07-04 UTC)

TIANHUI 5D, 60212

TIANHUI 5C, 60211

CZ-6A DEB, 60213

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CZ-6A 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.
6 mins	2025-12-20 14:15:08.019Z	26.989° NE	2025-12-20 14:18:08.019Z	109.597° ESE	38.522°	2025-12-20 14:21:08.019Z	174.975° S

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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-6A R/B, 60214 on other resources

View CZ-6A R/B, 60214 on Heavens-Above

View CZ-6A R/B, 60214 on Keep Track

View CZ-6A R/B, 60214 on Celestrak

View CZ-6A R/B, 60214 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-6A R/B, 60214

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2025-12-19T12:16:46.274Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #126 in the year 2024 (2024-07-04 UTC)

CZ-6A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-6A R/B, 60214 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 15 hours ago