CZ-7A R/B, 64063

Orbit data source: Space-Track

CZ-7A R/B, 64063 is space debris in HEO originally from a launch on Tue, 20 May 2025 UTC launched from the Wenchang Satellite Launch Center (WSC). 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/64063?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

64063, 2025-106B

Orbit

HEO

Country

CN / PRC

Related business

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

Manufacturer

CALT

Mission

Spacecraft

Bus & Motor

CZ-3A STAGE 3, Unknown motor

Mass

~2,800 kg wet, ~2,800 kg dry

Launch date (UTC)

2025-05-20 (9 months ago)

Launch vehicle

Unknown

Launch site

Wenchang Satellite Launch Center (WSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 1 Nozzle, 6.2 m

Radar Cross Section

32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago

0 CZ-7A R/B
1 64063U 25106B   26060.81805112  .00041594  93396-7  17276-2 0  9998
2 64063  15.6109 289.8036 6836157  96.6400 338.7895  2.90315728  7928

Epoch: 2026-03-01T19:37Z

TLE epoch observation values (Epoch: 2026-03-01T19:37:59.616Z)

Latitude

-0.00001°

Longitude

-164.25861°

Altitude

5,606.493 km

Speed

6.878 km/s

True Right ascension

19h 19m 26s

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

02:20:43

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

28,576.1 km

Perigee altitude

190.447 km

Semi-major axis

20,761.411 km

Eccentricity

0.68362

Inclination

15.6109°

RAAN

289.8036°

Arg. of periapsis

96.64°

True anomaly

263.09738°

Mean anomaly

338.7895°

Eccentric anomaly

307.8697°

Mean motion

0.72553 °/min

Orbital period

496.19 mins

BSTAR

0.0017276

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Other satellites on launch #106 in the year 2025 (2025-05-20 UTC)

CHINASAT 3B, 64062

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CZ-7A 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.
430 mins	2026-03-05 07:27:24.931Z	215.595° SW	2026-03-05 14:02:24.931Z	187.674° SSW	22.826°	2026-03-05 14:37:24.931Z	141.265° SSE

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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-7A R/B, 64063 on other resources

View CZ-7A R/B, 64063 on Heavens-Above

View CZ-7A R/B, 64063 on Keep Track

View CZ-7A R/B, 64063 on Celestrak

View CZ-7A R/B, 64063 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-7A R/B, 64063

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-03-01T19:37:59.616Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #106 in the year 2025 (2025-05-20 UTC)

CZ-7A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-7A R/B, 64063 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago