SHIYAN 6 02 (SY-6 02), 45859
Orbit data source: Space-Track
SHIYAN 6 02 (SY-6 02), 45859 is a payload satellite owned by CNSA (CN) in SSO that was launched on Sat, 04 Jul 2020 UTC via a CHANG ZHENG 2D 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.
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45859 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH Shenzhen
Mission
Operational Defense Technology
Bus & Motor
SW6, AOCS
Mass
~1,000 kg wet, ~900 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, Unknown HBR
Radar Cross Section
3.315 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 SHIYAN 6 02 (SY-6 02)
1 45859U 20043A 26172.54498683 .00000128 00000-0 33292-4 0 9999
2 45859 98.1842 183.8092 0128107 212.4661 146.8614 14.60934447317493Epoch: 2026-06-21T13:04Z
TLE epoch observation values (Epoch: 2026-06-21T13:04:46.862Z)
Latitude
0.00002°
Longitude
77.87021°
Altitude
769.324 km
Speed
7.429 km/s
True Right ascension
12h 15m 14s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:07:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
777.749 km
Perigee altitude
596.724 km
Semi-major axis
7,065.374 km
Eccentricity
0.01281
Inclination
98.1842°
RAAN
183.8092°
Arg. of periapsis
212.4661°
True anomaly
147.65326°
Mean anomaly
146.8614°
Eccentric anomaly
147.25838°
Mean motion
3.65461 °/min
Orbital period
98.51 mins
BSTAR
0.000033292
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Other satellites on launch #43 in the year 2020 (2020-07-04 UTC)
No other RSOs were in this launch
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SHIYAN 6 02 (SY-6 02) 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 12:42:09.994Z | 52.533° ENE | 2026-06-22 12:45:09.994Z | 100.682° ESE | 19.135° | 2026-06-22 12:47:09.994Z | 132.382° SE |
| 6 mins | 2026-06-22 14:20:09.994Z | 339.239° N | 2026-06-22 14:22:09.994Z | 296.72° NW | 29.691° | 2026-06-22 14:26:09.994Z | 226.447° WSW |
| 6 mins | 2026-06-22 23:46:09.994Z | 101.04° ESE | 2026-06-22 23:48:09.994Z | 68.981° E | 22.644° | 2026-06-22 23:52:09.994Z | 14.97° NNE |
| 8 mins | 2026-06-23 01:22:09.994Z | 201.012° SSW | 2026-06-23 01:25:09.994Z | 251.566° W | 32.556° | 2026-06-23 01:30:09.994Z | 330.909° NNW |
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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