CZ-7A R/B, 63398

Orbit data source: Space-Track

CZ-7A R/B, 63398 is space debris in HEO originally from a launch on Sat, 29 Mar 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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https://www.satcat.com/sats-embedded/63398?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

63398, 2025-064B

Orbit

HEO

Last TLE update

2 days 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)

2025-03-29 (1 month ago)

Launch vehicle

Unknown

Launch site

Wenchang Satellite Launch Center (WSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history

TLE from 2 days ago

0 CZ-7A R/B
1 63398U 25064B   25118.75761463  .00240130 -59450-5  26769-3 0  9994
2 63398  19.6388  76.4068 7126874 202.5445  95.9862  2.55384379   740

Epoch: 2025-04-28T18:10Z

Definitive object data (Epoch: 2025-04-28T18:10:57.904Z)

Latitude

-0.00007°

Longitude

-53.36432°

Altitude

26,188.933 km

Speed

2.617 km/s

True Right ascension

05h 05m 22s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

9.95347°

Longitude

-25.0221°

Altitude

31,610.52 km

Speed

1.817 km/s

Apparent Right ascension

06h 28m 51s

Apparent Declination

3° 46' 45"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:55:32

Azimuth

277.186° WNW

Elevation

-2.673°

Doppler factor

Orbital elements

Apogee altitude

32,351.257 km

Perigee altitude

118.929 km

Semi-major axis

22,613.23 km

Eccentricity

0.7126874

Inclination

19.6388°

RAAN

76.4068°

Arg. of periapsis

202.5445°

True anomaly

157.46146°

Mean anomaly

95.9862°

Eccentric anomaly

128.11381°

Mean motion

0.63826 °/min

BSTAR

0.00026769

Orbital period

564.03 mins

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Other satellites on launch #64 in the year 2025 (2025-03-29 UTC)

TJS-16, 63397

CZ-7A 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.
501 mins	2025-05-01 19:19:26.460Z	194.075° SSW	2025-05-02 03:03:26.460Z	194.247° SSW	40.494°	2025-05-02 03:40:26.460Z	119.415° SE

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Check out CZ-7A R/B, 63398 on other resources

View CZ-7A R/B, 63398 on Heavens-Above

View CZ-7A R/B, 63398 on Keep Track

View CZ-7A R/B, 63398 on Celestrak

View CZ-7A R/B, 63398 on Gunter's Space Page

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