CZ-3B R/B, 63076

Orbit data source: Space-Track

CZ-3B R/B, 63076 is space debris in HEO originally from a launch on Sat, 22 Feb 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/63076?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

63076, 2025-036B

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)

2025-02-22 (5 months ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

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

TLE from 2 days ago

0 CZ-3B R/B
1 63076U 25036B   25212.35971084  .00006190  00000-0  12795-2 0  9999
2 63076  27.3587 270.4277 7222803 281.0968  11.9325  2.36164257  3733

Epoch: 2025-07-31T08:37Z

TLE epoch observation values (Epoch: 2025-07-31T08:37:59.016Z)

Latitude

0.00022°

Longitude

-168.18611°

Altitude

3,665.293 km

Speed

7.914 km/s

True Right ascension

18h 02m 08s

True Declination

0° 00' 01"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

26.65197°

Longitude

-64.9426°

Altitude

34,618.921 km

Speed

1.647 km/s

Apparent Right ascension

00h 24m 35s

Apparent Declination

21° 48' 19"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

05:57:45

Azimuth

283.142° WNW

Elevation

18.756°

Doppler factor

Orbital elements

Apogee altitude

34,651.669 km

Perigee altitude

237.967 km

Semi-major axis

23,822.955 km

Eccentricity

0.72228

Inclination

27.3587°

RAAN

270.4277°

Arg. of periapsis

281.0968°

True anomaly

78.97374°

Mean anomaly

11.9325°

Eccentric anomaly

36.61532°

Mean motion

0.59027 °/min

Orbital period

609.89 mins

BSTAR

0.0012795

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Other satellites on launch #36 in the year 2025 (2025-02-22 UTC)

CHINASAT 10R, 63075

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.
92 mins	2025-08-02 16:12:12.150Z	283.126° WNW	2025-08-02 16:12:12.150Z	283.126° WNW	17.821°	2025-08-02 17:44:12.150Z	285.873° WNW
497 mins	2025-08-03 07:55:12.150Z	239.117° WSW	2025-08-03 10:19:12.150Z	217.302° SW	43.44°	2025-08-03 16:12:12.150Z	236.351° WSW

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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Authenticating...

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Check out CZ-3B R/B, 63076 on other resources

View CZ-3B R/B, 63076 on Heavens-Above

View CZ-3B R/B, 63076 on Keep Track

View CZ-3B R/B, 63076 on Celestrak

View CZ-3B R/B, 63076 on Gunter's Space Page

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