HAIYANG 1C, 43609
Orbit data source: Space-Track
HAIYANG 1C, 43609 is a Chinese payload satellite in SSO that was launched on Fri, 07 Sep 2018 UTC via a CHANG ZHENG 2C launch vehicle from the Taiyaun Space Center, China (TSC). 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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43609 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Operational Civil Imaging
Bus & Motor
CAST-968, Unknown motor
Mass
442 kg wet, 429 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.8 m
Radar Cross Section
3.660 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 HAIYANG 1C
1 43609U 18068A 25287.94213184 .00000230 00000-0 97755-4 0 9993
2 43609 98.5500 358.4389 0011708 102.8144 257.4350 14.34159683371931Epoch: 2025-10-14T22:36Z
TLE epoch observation values (Epoch: 2025-10-14T22:36:40.190Z)
Latitude
-0.00002°
Longitude
-4.45188°
Altitude
782.632 km
Speed
7.462 km/s
True Right ascension
23h 53m 45s
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
05:12:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
783.367 km
Perigee altitude
766.617 km
Semi-major axis
7,153.129 km
Eccentricity
0.00117
Inclination
98.55°
RAAN
358.4389°
Arg. of periapsis
102.8144°
True anomaly
257.30409°
Mean anomaly
257.435°
Eccentric anomaly
257.36954°
Mean motion
3.58756 °/min
Orbital period
100.35 mins
BSTAR
0.000097755
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Other satellites on launch #68 in the year 2018 (2018-09-07 UTC)
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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.HAIYANG 1C 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-15 17:36:10.850Z | 16.9° NNE | 2025-10-15 17:41:10.850Z | 152.612° SSE | 43.321° | 2025-10-15 17:45:10.850Z | 188.752° SSW |
| 9 mins | 2025-10-16 04:52:10.850Z | 170.291° S | 2025-10-16 04:56:10.850Z | 249.805° W | 44.568° | 2025-10-16 05:01:10.850Z | 344.342° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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