CZ-6A R/B, 61570

Orbit data source: Space-Track

CZ-6A R/B, 61570 is space debris in LEO originally from a launch on Tue, 15 Oct 2024 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/61570?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61570, 2024-185U

Orbit

LEO

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)

2024-10-15 (1 year 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
Last TLE update: 11 hours ago

TLE from 11 hours ago

0 CZ-6A R/B
1 61570U 24185U   25335.44907602  .00000624  00000-0  14172-3 0  9999
2 61570  89.0215  78.2535 0099738 150.5461 210.1419 14.51627797 58970

Epoch: 2025-12-01T10:46Z

TLE epoch observation values (Epoch: 2025-12-01T10:46:40.168Z)

Latitude

-0.00005°

Longitude

-153.96229°

Altitude

784.851 km

Speed

7.429 km/s

True Right ascension

05h 13m 00s

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

19:06:55

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

788.01 km

Perigee altitude

646.474 km

Semi-major axis

7,095.379 km

Eccentricity

0.00997

Inclination

89.0215°

RAAN

78.2535°

Arg. of periapsis

150.5461°

True anomaly

209.57413°

Mean anomaly

210.1419°

Eccentric anomaly

209.8574°

Mean motion

3.63145 °/min

Orbital period

99.13 mins

BSTAR

0.00014172

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Other satellites on launch #185 in the year 2024 (2024-10-15 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.
8 mins	2025-12-02 06:45:27.375Z	140.629° SSE	2025-12-02 06:49:27.375Z	73.727° E	29.09°	2025-12-02 06:53:27.375Z	18.69° NNE
6 mins	2025-12-02 08:25:27.375Z	233.23° WSW	2025-12-02 08:28:27.375Z	279.088° WNW	22.215°	2025-12-02 08:31:27.375Z	323.668° NNW
6 mins	2025-12-02 18:48:27.375Z	27.094° NE	2025-12-02 18:51:27.375Z	98.34° ESE	32.451°	2025-12-02 18:54:27.375Z	151.778° SSE
4 mins	2025-12-02 20:28:27.375Z	306.216° NW	2025-12-02 20:30:27.375Z	274.806° WNW	15.641°	2025-12-02 20:32:27.375Z	247.178° WSW

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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, 61570 on other resources

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View CZ-6A R/B, 61570 on Keep Track

View CZ-6A R/B, 61570 on Celestrak

View CZ-6A R/B, 61570 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-6A R/B, 61570

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: 2025-12-01T10:46:40.168Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #185 in the year 2024 (2024-10-15 UTC)

CZ-6A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-6A R/B, 61570 on other resources

Documentation

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