CZ-3B R/B, 63525

Orbit data source: Space-Track

CZ-3B R/B, 63525 is space debris in HEO originally from a launch on Thu, 10 Apr 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 URL

https://www.satcat.com/sats-embedded/63525?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

63525, 2025-073B

Orbit

HEO

Last TLE update

23 hours ago

Origin

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

Manufacturer

CALT

Mission

Spacecraft

Bus & Motor

CZ-3A STAGE 3, Unknown motor

Mass

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

Launch date (UTC)

2025-04-10 (1 month ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history

TLE from 23 hours ago

0 CZ-3B R/B
1 63525U 25073B   25128.92148781  .00096134 -39505-6  77670-3 0  9998
2 63525  19.1894  77.1798 7331592 200.1294  99.7704  2.27084400   634

Epoch: 2025-05-08T22:06Z

Definitive object data (Epoch: 2025-05-08T22:06:56.546Z)

Latitude

-0.00005°

Longitude

-121.6014°

Altitude

29,927.74 km

Speed

2.378 km/s

True Right ascension

05h 08m 28s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

6.03019°

Longitude

-104.29404°

Altitude

35,879.822 km

Speed

1.598 km/s

Apparent Right ascension

06h 23m 53s

Apparent Declination

0° 33' 36"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

05:30:19

Azimuth

159.418° S

Elevation

48.796°

Doppler factor

Orbital elements

Apogee altitude

36,005.766 km

Perigee altitude

147.377 km

Semi-major axis

24,454.708 km

Eccentricity

0.7331592

Inclination

19.1894°

RAAN

77.1798°

Arg. of periapsis

200.1294°

True anomaly

159.86977°

Mean anomaly

99.7704°

Eccentric anomaly

131.31934°

Mean motion

0.56754 °/min

BSTAR

0.0007767

Orbital period

634.31 mins

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Other satellites on launch #73 in the year 2025 (2025-04-10 UTC)

TJS-17, 63524

TJS-17 AKM, 63629

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.
313 mins	2025-05-09 21:19:03.171Z	159.427° S	2025-05-10 01:44:03.171Z	186.196° SSW	40.697°	2025-05-10 02:32:03.171Z	114.471° SE
268 mins	2025-05-10 16:51:03.171Z	104.481° ESE	2025-05-10 21:19:03.171Z	120.197° SE	33.253°	2025-05-10 21:19:03.171Z	120.197° SE

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Check out CZ-3B R/B, 63525 on other resources

View CZ-3B R/B, 63525 on Heavens-Above

View CZ-3B R/B, 63525 on Keep Track

View CZ-3B R/B, 63525 on Celestrak

View CZ-3B R/B, 63525 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.