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: 11 hours ago
TLE from 11 hours ago
0 ZHUHAI-1 03E
1 44539U 19060F 25259.29664566 .00016225 00000-0 56720-3 0 9997
2 44539 97.5322 37.6390 0009924 267.5905 92.4199 15.29584720333737Epoch: 2025-09-16T07:07Z
TLE epoch observation values (Epoch: 2025-09-16T07:07:10.185Z)
Latitude
0.00003°
Longitude
-64.64242°
Altitude
480.446 km
Speed
7.625 km/s
True Right ascension
02h 30m 33s
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
11:08:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.811 km
Perigee altitude
467.211 km
Semi-major axis
6,852.148 km
Eccentricity
0.00099
Inclination
97.5322°
RAAN
37.639°
Arg. of periapsis
267.5905°
True anomaly
92.53351°
Mean anomaly
92.4199°
Eccentric anomaly
92.47671°
Mean motion
3.82651 °/min
Orbital period
94.08 mins
BSTAR
0.0005672
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-16 21:48:56.098Z | 29.86° NE | 2025-09-16 21:51:56.098Z | 106.879° ESE | 33.567° | 2025-09-16 21:54:56.098Z | 170.225° S |
| 5 mins | 2025-09-17 09:56:56.098Z | 214.68° SW | 2025-09-17 09:58:56.098Z | 265.959° W | 25.645° | 2025-09-17 10:01:56.098Z | 324.457° NNW |
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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