ZHUHAI-1 02, 42759 (Decayed)
Orbit data source: Space-Track
ZHUHAI-1 02, 42759 was a payload satellite owned by Zhuhai Orbita (CN) in LEO that was launched on Thu, 15 Jun 2017 UTC via a CHANG ZHENG 4B 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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42759 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Zhuhai Orbita
Mission
Decayed Commercial Imaging
Bus & Motor
OVS-1, Unknown motor
Mass
50 kg wet, 50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.5 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 ZHUHAI-1 02
1 42759U 17034B 25286.97241530 .03437790 89859-5 10544-2 0 9999
2 42759 42.9888 273.3261 0008257 129.3938 230.7682 16.25684504462550Epoch: 2025-10-13T23:20Z
TLE epoch observation values (Epoch: 2025-10-13T23:20:16.681Z)
Latitude
-0.00003°
Longitude
-99.51096°
Altitude
207.367 km
Speed
7.782 km/s
True Right ascension
18h 13m 18s
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
12:53:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
211.629 km
Perigee altitude
200.755 km
Semi-major axis
6,584.329 km
Eccentricity
0.00083
Inclination
42.9888°
RAAN
273.3261°
Arg. of periapsis
129.3938°
True anomaly
230.69496°
Mean anomaly
230.7682°
Eccentric anomaly
230.73157°
Mean motion
4.06234 °/min
Orbital period
88.62 mins
BSTAR
0.0010544
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Other satellites on launch #34 in the year 2017 (2017-06-15 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 02 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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