Showing default

SHIYAN 23 (SY-23), 59728

Orbit data source: Space-Track

SHIYAN 23 (SY-23), 59728 is a payload satellite owned by CNSA (CN) in SSO that was launched on Sat, 11 May 2024 UTC via a CHANG ZHENG 4C 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.

Loading next visibility...
Identifier
59728, 2024-089A
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CAST
Mission
Operational Defense Technology
Bus & Motor
SY23, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
2024-05-11 (2 years ago)
Launch vehicle
CHANG ZHENG 4C
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
4.795 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 SHIYAN 23 (SY-23)
1 59728U 24089A   26311.72009389  .00000481  00000-0  59404-4 0  9994
2 59728  97.7827 310.6202 0005403  85.2131 274.9702 14.87182119135179
Epoch: 2026-11-07T17:16Z
TLE epoch observation values (Epoch: 2026-11-07T17:16:56.112Z)
Latitude
-0.00001°
Longitude
4.4651°
Altitude
609.455 km
Speed
7.555 km/s
True Right ascension
20h 42m 28s
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
00:52:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
607.543 km
Perigee altitude
599.999 km
Semi-major axis
6,981.908 km
Eccentricity
0.00054
Inclination
97.7827°
RAAN
310.6202°
Arg. of periapsis
85.2131°
True anomaly
274.90852°
Mean anomaly
274.9702°
Eccentric anomaly
274.93936°
Mean motion
3.72033 °/min
Orbital period
96.77 mins
BSTAR
0.000059404
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #89 in the year 2024 (2024-05-11 UTC)

Documentation

Showing up to 5 results
|