ZHUHAI-1 03E, 44539
Orbit data source: Space-Track
ZHUHAI-1 03E, 44539 is a payload satellite owned by Zhuhai Orbita (CN) in SSO that was launched on Thu, 19 Sep 2019 UTC via a CHANG ZHENG 11 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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44539 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Harbin
Mission
Operational Commercial Imaging
Bus & Motor
OVS-1, Unknown motor
Mass
95 kg wet, 95 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, Unknown HBR
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ZHUHAI-1 03E
1 44539U 19060F 25292.96992872 .00027731 00000-0 91755-3 0 9993
2 44539 97.5365 71.8055 0011038 147.7100 212.4819 15.31244027338887Epoch: 2025-10-19T23:16Z
TLE epoch observation values (Epoch: 2025-10-19T23:16:41.841Z)
Latitude
0.00002°
Longitude
53.9522°
Altitude
481.584 km
Speed
7.621 km/s
True Right ascension
04h 47m 13s
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
00:38:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.614 km
Perigee altitude
461.498 km
Semi-major axis
6,847.193 km
Eccentricity
0.0011
Inclination
97.5365°
RAAN
71.8055°
Arg. of periapsis
147.71°
True anomaly
212.41405°
Mean anomaly
212.4819°
Eccentric anomaly
212.44797°
Mean motion
3.83067 °/min
Orbital period
93.98 mins
BSTAR
0.00091755
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Other satellites on launch #60 in the year 2019 (2019-09-19 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.ZHUHAI-1 03E 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 | 2025-10-20 08:49:57.397Z | 125.528° SE | 2025-10-20 08:51:57.397Z | 83.056° E | 25.109° | 2025-10-20 08:54:57.397Z | 14.498° NNE |
| 5 mins | 2025-10-20 21:48:57.397Z | 44.131° NE | 2025-10-20 21:50:57.397Z | 104.443° ESE | 29.634° | 2025-10-20 21:53:57.397Z | 165.671° S |
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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