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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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 (2 years 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: 10 hours ago

TLE from 10 hours ago

0 CZ-6A R/B
1 61570U 24185U   26169.24020730  .00000200  00000-0  42511-4 0  9990
2 61570  89.0231  54.9755 0097740 190.8733 169.0364 14.51785979 87816

Epoch: 2026-06-18T05:45Z

TLE epoch observation values (Epoch: 2026-06-18T05:45:53.910Z)

Latitude

-0.00007°

Longitude

62.0145°

Altitude

791.068 km

Speed

7.422 km/s

True Right ascension

03h 39m 54s

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

02:16:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

786.072 km

Perigee altitude

647.381 km

Semi-major axis

7,094.864 km

Eccentricity

0.00977

Inclination

89.0231°

RAAN

54.9755°

Arg. of periapsis

190.8733°

True anomaly

169.24688°

Mean anomaly

169.0364°

Eccentric anomaly

169.14189°

Mean motion

3.63184 °/min

Orbital period

99.12 mins

BSTAR

0.000042511

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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.
7 mins	2026-06-18 15:49:39.966Z	123.162° SE	2026-06-18 15:52:39.966Z	83.914° E	20.964°	2026-06-18 15:56:39.966Z	30.282° NE
8 mins	2026-06-18 17:28:39.966Z	214.403° SW	2026-06-18 17:31:39.966Z	267.199° W	32.603°	2026-06-18 17:36:39.966Z	343.194° N
5 mins	2026-06-19 03:52:39.966Z	42.793° NE	2026-06-19 03:54:39.966Z	77.458° E	22.791°	2026-06-19 03:57:39.966Z	129.134° SE
6 mins	2026-06-19 05:31:39.966Z	323.796° NNW	2026-06-19 05:33:39.966Z	288.802° WNW	24.754°	2026-06-19 05:37:39.966Z	223.545° 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, 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

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CZ-6A R/B, 61570

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-06-18T05:45:53.910Z)

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: 10 hours ago