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

Last TLE update

9 hours ago

Origin

China National Space Administration (CN / PRC)

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 (3 months ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 5.5 m

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history

TLE from 9 hours ago

0 CZ-6A R/B
1 63605U 25078G   25199.60287707  .00000207  00000-0  18234-3 0  9995
2 63605  99.7000 212.6416 0105643 225.9490 133.2932 13.94753351 12613

Epoch: 2025-07-18T14:28Z

TLE epoch observation values (Epoch: 2025-07-18T14:28:08.578Z)

Latitude

-0.00009°

Longitude

58.9539°

Altitude

968.115 km

Speed

7.341 km/s

True Right ascension

14h 10m 33s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

19.7768°

Longitude

-117.13039°

Altitude

881.189 km

Speed

7.43 km/s

Apparent Right ascension

01h 41m 30s

Apparent Declination

-8° 06' 52"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:38:44

Azimuth

331.986° NNW

Elevation

-55.243°

Doppler factor

Orbital elements

Apogee altitude

986.248 km

Perigee altitude

832.275 km

Semi-major axis

7,287.399 km

Eccentricity

0.01056

Inclination

99.7°

RAAN

212.6416°

Arg. of periapsis

225.949°

True anomaly

134.16638°

Mean anomaly

133.2932°

Eccentric anomaly

133.73058°

Mean motion

3.48887 °/min

Orbital period

103.19 mins

BSTAR

0.00018234

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

CZ-6A 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.
11 mins	2025-07-19 00:54:03.585Z	168.921° S	2025-07-19 01:00:03.585Z	297.882° NW	44.041°	2025-07-19 01:05:03.585Z	342.022° N
9 mins	2025-07-19 13:28:03.585Z	30.224° NE	2025-07-19 13:32:03.585Z	107.41° ESE	39.29°	2025-07-19 13:37:03.585Z	178.052° S
7 mins	2025-07-19 15:10:03.585Z	338.738° N	2025-07-19 15:13:03.585Z	302.344° NW	20.571°	2025-07-19 15:17:03.585Z	253.952° W
6 mins	2025-07-19 23:22:03.585Z	89.251° E	2025-07-19 23:25:03.585Z	53.831° ENE	18.478°	2025-07-19 23:28:03.585Z	21.829° NNE

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-6A R/B, 63605 on other resources

View CZ-6A R/B, 63605 on Heavens-Above

View CZ-6A R/B, 63605 on Keep Track

View CZ-6A R/B, 63605 on Celestrak

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

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