CZ-6A R/B, 63921

Orbit data source: Space-Track

CZ-6A R/B, 63921 is space debris in LEO originally from a launch on Sun, 11 May 2025 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/63921?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

63921, 2025-096D

Orbit

LEO

Country

CN / PRC

Related business

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

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2025-05-11 (10 months ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 3.3 m

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago

0 CZ-6A R/B
1 63921U 25096D   26061.80365892  .00000491  00000-0  19568-3 0  9995
2 63921  85.9890 232.5681 0014451  39.4207 320.8033 14.26529039 41958

Epoch: 2026-03-02T19:17Z

TLE epoch observation values (Epoch: 2026-03-02T19:17:16.130Z)

Latitude

0.00001°

Longitude

142.65907°

Altitude

798.352 km

Speed

7.458 km/s

True Right ascension

15h 30m 16s

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

07:14:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

810.714 km

Perigee altitude

789.967 km

Semi-major axis

7,178.477 km

Eccentricity

0.00145

Inclination

85.989°

RAAN

232.5681°

Arg. of periapsis

39.4207°

True anomaly

320.6985°

Mean anomaly

320.8033°

Eccentric anomaly

320.75091°

Mean motion

3.56857 °/min

Orbital period

100.88 mins

BSTAR

0.00019568

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Other satellites on launch #96 in the year 2025 (2025-05-11 UTC)

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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.
5 mins	2026-03-03 10:35:09.792Z	111.251° ESE	2026-03-03 10:38:09.792Z	74.644° E	15.13°	2026-03-03 10:40:09.792Z	50.351° ENE
8 mins	2026-03-03 12:15:09.792Z	202.869° SW	2026-03-03 12:18:09.792Z	254.796° W	39.494°	2026-03-03 12:23:09.792Z	352.943° N
8 mins	2026-03-03 22:49:09.792Z	22.109° NNE	2026-03-03 22:52:09.792Z	75.633° E	33.424°	2026-03-03 22:57:09.792Z	151.358° SSE
6 mins	2026-03-04 00:31:09.792Z	310.6° NW	2026-03-04 00:33:09.792Z	281.711° WNW	20.6°	2026-03-04 00:37:09.792Z	230.929° WSW

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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, 63921 on other resources

View CZ-6A R/B, 63921 on Heavens-Above

View CZ-6A R/B, 63921 on Keep Track

View CZ-6A R/B, 63921 on Celestrak

View CZ-6A R/B, 63921 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, 63921

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-03-02T19:17:16.130Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #96 in the year 2025 (2025-05-11 UTC)

CZ-6A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-6A R/B, 63921 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago