HAIWANGXING 01 (NEPTUNE), 59677 (Decayed)
Orbit data source: Space-Track
HAIWANGXING 01 (NEPTUNE), 59677 was a Chinese payload satellite in LEO that was launched on Tue, 07 May 2024 UTC via a CHANG ZHENG 6C 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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59677 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Decayed Commercial Radar Imaging
Bus & Motor
HWX, Unknown motor
Mass
239 kg wet, ~239 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 HAIWANGXING 01 (NEPTUNE)
1 59677U 24085A 25087.75342935 .29817615 25160-5 69315-3 0 9998
2 59677 97.3281 172.1165 0011504 275.3276 181.9815 16.45520891 50135Epoch: 2025-03-28T18:04Z
TLE epoch observation values (Epoch: 2025-03-28T18:04:56.295Z)
Latitude
79.71897°
Longitude
-60.70392°
Altitude
172.005 km
Speed
7.805 km/s
True Right ascension
02h 27m 45s
True Declination
79° 39' 11"
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
21:39:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
155.462 km
Perigee altitude
140.447 km
Semi-major axis
6,526.091 km
Eccentricity
0.00115
Inclination
97.3281°
RAAN
172.1165°
Arg. of periapsis
275.3276°
True anomaly
181.97695°
Mean anomaly
181.9815°
Eccentric anomaly
181.97922°
Mean motion
4.11683 °/min
Orbital period
87.45 mins
BSTAR
0.00069315
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Other satellites on launch #85 in the year 2024 (2024-05-07 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.HAIWANGXING 01 (NEPTUNE) Visibility
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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. |
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| This satellite is decayed. |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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