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

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)

2025-02-22 (1 year ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 1 Nozzle, 4.2 m

Radar Cross Section

32.704 m², Large (>1 m²)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 CZ-3B R/B
1 63076U 25036B   26093.37213546  .00050743  85577-7  63673-3 0  9995
2 63076  26.8860 172.2856 7181261  83.3877 346.5311  2.46154489  9620

Epoch: 2026-04-03T08:55Z

TLE epoch observation values (Epoch: 2026-04-03T08:55:52.503Z)

Latitude

-0.00001°

Longitude

-153.28841°

Altitude

3,971.906 km

Speed

7.734 km/s

True Right ascension

11h 29m 33s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

19:12:32

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

33,437.951 km

Perigee altitude

154.047 km

Semi-major axis

23,174.136 km

Eccentricity

0.71813

Inclination

26.886°

RAAN

172.2856°

Arg. of periapsis

83.3877°

True anomaly

276.40143°

Mean anomaly

346.5311°

Eccentric anomaly

320.18529°

Mean motion

0.61523 °/min

Orbital period

585.15 mins

BSTAR

0.00063673

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

CHINASAT 10R, 63075

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CZ-3B 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.
12 mins	2026-04-04 14:40:31.008Z	200.128° SSW	2026-04-04 14:43:31.008Z	169.208° S	15.981°	2026-04-04 14:52:31.008Z	136.518° 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-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

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

CZ-3B R/B, 63076

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-04-03T08:55:52.503Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

CZ-3B R/B Visibility forecast

Co-orbital & Co-planar RSOs

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

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago