DECAYED

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SZ-17 MODULE, 59624 (Decayed)

Orbit data source: Space-Track

SZ-17 MODULE, 59624 was a payload satellite in LEO that was launched on Thu, 26 Oct 2023 UTC launched 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.

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Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/59624?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/59624?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59624, 2023-164C

Orbit

Decayed

Last TLE update

5 months ago

Origin

China Manned Space Agency (CN)

Manufacturer

CAST

Mission

Decayed spacecraft

Bus & Motor

SHENZHOU OM, Unknown motor

Mass

~1,842 kg wet, ~1,500 kg dry

Launch date (UTC)

2023-10-26 (2 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history

TLE from 5 months ago

0 SZ-17 MODULE
1 59624U 23164C   24353.36152807  .07140113  81950-5  30278-3 0  9999
2 59624  41.4570   6.9151 0001794 173.2499 274.5824 16.43931394 36708

Epoch: 2024-12-18T08:40Z

TLE epoch observation values (Epoch: 2024-12-18T08:40:36.025Z)

Latitude

41.58441°

Longitude

-123.61359°

Altitude

157.817 km

Speed

7.818 km/s

True Right ascension

06h 15m 58s

True Declination

41° 23' 53"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

158.851 km

Perigee altitude

156.506 km

Semi-major axis

6,535.816 km

Eccentricity

0.00018

Inclination

41.457°

RAAN

6.9151°

Arg. of periapsis

173.2499°

True anomaly

Unknown

Mean anomaly

274.5824°

Eccentric anomaly

Unknown

Mean motion

4.10765 °/min

Orbital period

87.64 mins

BSTAR

0.00030278

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

SZ-17, 58146 (Decayed)

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

SZ-17 MODULE Visibility

Observer location: undefined°, undefined°

This satellite is decayed

Authenticating...

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Check out SZ-17 MODULE, 59624 (Decayed) on other resources

View SZ-17 MODULE, 59624 (Decayed) on Celestrak

View SZ-17 MODULE, 59624 (Decayed) on Gunter's Space Page

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