CZ-6A R/B, 64961

Orbit data source: Space-Track

CZ-6A R/B, 64961 is space debris in LEO originally from a launch on Sun, 27 Jul 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/64961?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

64961, 2025-159F

Orbit

LEO

Last TLE update

16 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)

2025-07-27 (2 weeks ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history

TLE from 16 hours ago

0 CZ-6A R/B
1 64961U 25159F   25224.76106849  .00000067  00000-0  34723-4 0  9990
2 64961  86.5063  26.7914 0104675  66.4157 294.7967 13.94024890  2250

Epoch: 2025-08-12T18:15Z

TLE epoch observation values (Epoch: 2025-08-12T18:15:56.317Z)

Latitude

-0.00007°

Longitude

151.35766°

Altitude

886.196 km

Speed

7.425 km/s

True Right ascension

01h 47m 09s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

5.76089°

Longitude

-29.25147°

Altitude

942.158 km

Speed

7.368 km/s

Apparent Right ascension

13h 28m 10s

Apparent Declination

-15° 23' 25"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

01:03:31

Azimuth

345.884° N

Elevation

-64.891°

Doppler factor

Orbital elements

Apogee altitude

987.884 km

Perigee altitude

835.274 km

Semi-major axis

7,289.716 km

Eccentricity

0.01047

Inclination

86.5063°

RAAN

26.7914°

Arg. of periapsis

66.4157°

True anomaly

293.70186°

Mean anomaly

294.7967°

Eccentric anomaly

294.24988°

Mean motion

3.4872 °/min

Orbital period

103.23 mins

BSTAR

0.000034723

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Other satellites on launch #159 in the year 2025 (2025-07-27 UTC)

CZ-6A R/B Visibility forecast

Observer location: undefined°, undefined°
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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.
10 mins	2025-08-13 11:35:30.868Z	188.807° SSW	2025-08-13 11:40:30.868Z	244.258° WSW	43.161°	2025-08-13 11:45:30.868Z	356.857° N
9 mins	2025-08-13 22:25:30.868Z	19.899° NNE	2025-08-13 22:29:30.868Z	95.808° ESE	35.126°	2025-08-13 22:34:30.868Z	155.122° SSE
7 mins	2025-08-14 00:09:30.868Z	316.592° NNW	2025-08-14 00:12:30.868Z	276.666° WNW	21.269°	2025-08-14 00:16:30.868Z	231.32° WSW
5 mins	2025-08-14 10:02:30.868Z	107.662° ESE	2025-08-14 10:04:30.868Z	83.409° E	16.434°	2025-08-14 10:07:30.868Z	46.603° ENE

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, 64961 on other resources

View CZ-6A R/B, 64961 on Heavens-Above

View CZ-6A R/B, 64961 on Keep Track

View CZ-6A R/B, 64961 on Celestrak

View CZ-6A R/B, 64961 on Gunter's Space Page

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