CZ-6A R/B, 63605

Orbit data source: Space-Track

CZ-6A R/B, 63605 is space debris in SSO originally from a launch on Fri, 18 Apr 2025 UTC launched from the Taiyaun Space Center, China (TSC). 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/63605?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

63605, 2025-078G

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

CZ-6A STAGE 2, YF-115

Mass

~6,000 kg wet, ~6,000 kg dry

Launch date (UTC)

2025-04-18 (11 months ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 4.4 m

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago

0 CZ-6A R/B
1 63605U 25078G   26089.33184821 -.00000150  00000-0 -71669-4 0  9998
2 63605  99.6814 120.1096 0105489 263.6952  95.2184 13.94795131 48125

Epoch: 2026-03-30T07:57Z

TLE epoch observation values (Epoch: 2026-03-30T07:57:51.685Z)

Latitude

-0.00002°

Longitude

172.91934°

Altitude

922.521 km

Speed

7.387 km/s

True Right ascension

08h 00m 26s

True Declination

0° 00' 00"

Sunlit

Object was in daylight 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

00:08:39

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

985.988 km

Perigee altitude

832.243 km

Semi-major axis

7,287.252 km

Eccentricity

0.01055

Inclination

99.6814°

RAAN

120.1096°

Arg. of periapsis

263.6952°

True anomaly

96.42067°

Mean anomaly

95.2184°

Eccentric anomaly

95.81969°

Mean motion

3.48897 °/min

Orbital period

103.18 mins

BSTAR

-0.000071669

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Other satellites on launch #78 in the year 2025 (2025-04-18 UTC)

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CZ-6A 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.
11 mins	2026-03-31 01:17:29.459Z	140.918° SSE	2026-03-31 01:23:29.459Z	58.591° ENE	36.754°	2026-03-31 01:28:29.459Z	357.915° N
8 mins	2026-03-31 03:01:29.459Z	219.002° SW	2026-03-31 03:05:29.459Z	269.943° W	23.268°	2026-03-31 03:09:29.459Z	315.54° NNW
8 mins	2026-03-31 13:51:29.459Z	49.116° ENE	2026-03-31 13:55:29.459Z	99.845° ESE	22.803°	2026-03-31 13:59:29.459Z	145.833° SSE
10 mins	2026-03-31 15:32:29.459Z	359.989° N	2026-03-31 15:37:29.459Z	281.958° WNW	36.62°	2026-03-31 15:42:29.459Z	220.044° SW

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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-6A R/B, 63605 on other resources

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View CZ-6A R/B, 63605 on Gunter's Space Page

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CZ-6A R/B, 63605

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-03-30T07:57:51.685Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #78 in the year 2025 (2025-04-18 UTC)

CZ-6A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-6A R/B, 63605 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago