DECAYED

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SZ-17, 58146 (Decayed)

Orbit data source: Space-Track

SZ-17, 58146 was a payload satellite owned by ZZHGB (CN) in LEO that was launched on Thu, 26 Oct 2023 UTC via a CHANG ZHENG 2F launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Not visible in the next 10 days

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<iframe src="https://www.satcat.com/sats-embedded/58146?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/58146?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

58146, 2023-164A

Orbit

Decayed

Last TLE update

1 year ago

Origin

China Manned Space Agency (CN / PRC)

Manufacturer

CALT

Mission

Decayed Civil Spaceship

Bus & Motor

SHENZHOU, Unknown motor

Mass

~8,100 kg wet, 3,258 kg dry

Launch date (UTC)

2023-10-26 (2 years ago)

Launch vehicle

CHANG ZHENG 2F

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 2 Pan, 17 m

Radar Cross Section

39.234 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 year ago

0 SZ-17
1 58146U 23164A   24131.92201202  .00086906  00000-0  90008-3 0  9998
2 58146  41.4681 310.7607 0003738 318.2893  41.7661 15.63655876 29311

Epoch: 2024-05-10T22:07Z

TLE epoch observation values (Epoch: 2024-05-10T22:07:41.838Z)

Latitude

-0.00005°

Longitude

109.64075°

Altitude

374.823 km

Speed

7.688 km/s

True Right ascension

20h 43m 02s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

381.869 km

Perigee altitude

376.817 km

Semi-major axis

6,757.48 km

Eccentricity

0.00037

Inclination

41.4681°

RAAN

310.7607°

Arg. of periapsis

318.2893°

True anomaly

Unknown

Mean anomaly

41.7661°

Eccentric anomaly

Unknown

Mean motion

3.9072 °/min

Orbital period

92.14 mins

BSTAR

0.00090008

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Other satellites on launch #164 in the year 2023 (2023-10-26 UTC)

CZ-2F R/B, 58147 (Decayed)

SZ-17 MODULE, 59624 (Decayed)

SZ-17 Visibility

Observer location: undefined°, undefined°

This satellite is decayed

Authenticating...

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Check out SZ-17, 58146 (Decayed) on other resources

View SZ-17, 58146 (Decayed) on Celestrak

View SZ-17, 58146 (Decayed) on Gunter's Space Page

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