CZ-3B R/B, 64471

Orbit data source: Space-Track

CZ-3B R/B, 64471 is space debris in HEO originally from a launch on Fri, 20 Jun 2025 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 src="https://www.satcat.com/sats-embedded/64471?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/64471?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

64471, 2025-132B

Orbit

HEO

Last TLE update

1 week ago

Origin

CASC (CN / PRC)

Manufacturer

CALT

Mission

Operational spacecraft

Bus & Motor

CZ-3A STAGE 3, Unknown motor

Mass

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

Launch date (UTC)

2025-06-20 (2 weeks ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

RCS unknown

Expand to show TLE details & history

TLE from 1 week ago

0 CZ-3B R/B
1 64471U 25132B   25174.44696663  .00024482  11871-5  16405-2 0  9999
2 64471  27.6360  93.9323 7344542 181.4842 173.4852  2.23218496    89

Epoch: 2025-06-23T10:43Z

TLE epoch observation values (Epoch: 2025-06-23T10:43:37.916Z)

Latitude

0.00022°

Longitude

21.15566°

Altitude

36,501.514 km

Speed

1.573 km/s

True Right ascension

06h 15m 40s

True Declination

0° 00' 01"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

8.99704°

Longitude

35.71982°

Altitude

33,519.115 km

Speed

1.961 km/s

Apparent Right ascension

07h 42m 29s

Apparent Declination

3° 09' 11"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

01:35:53

Azimuth

86.524° E

Elevation

0.759°

Doppler factor

Orbital elements

Apogee altitude

36,524.032 km

Perigee altitude

190.206 km

Semi-major axis

24,735.256 km

Eccentricity

0.73445

Inclination

27.636°

RAAN

93.9323°

Arg. of periapsis

181.4842°

True anomaly

Unknown

Mean anomaly

173.4852°

Eccentric anomaly

Unknown

Mean motion

0.55792 °/min

Orbital period

645.26 mins

BSTAR

0.0016405

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Other satellites on launch #132 in the year 2025 (2025-06-20 UTC)

CHINASAT-9C, 64470

CZ-3B R/B Visibility forecast

Observer location: undefined°, undefined°

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.
272 mins	2025-07-01 19:19:52.072Z	225.13° WSW	2025-07-01 21:01:52.072Z	236.752° WSW	17.648°	2025-07-01 23:51:52.072Z	262.092° W
32 mins	2025-07-02 03:40:52.072Z	277.892° WNW	2025-07-02 04:06:52.072Z	238.485° WSW	21.235°	2025-07-02 04:12:52.072Z	189.859° SSW

Authenticating...

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Check out CZ-3B R/B, 64471 on other resources

View CZ-3B R/B, 64471 on Heavens-Above

View CZ-3B R/B, 64471 on Keep Track

View CZ-3B R/B, 64471 on Celestrak

View CZ-3B R/B, 64471 on Gunter's Space Page

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