ZHUHAI-1 OVS-02, 43440
Orbit data source: Space-Track
ZHUHAI-1 OVS-02, 43440 is a payload satellite owned by Zhuhai Orbita (CN) in SSO that was launched on Thu, 26 Apr 2018 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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43440 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, 0.5 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ZHUHAI-1 OVS-02
1 43440U 18040B 25309.97414854 .00008770 00000-0 39178-3 0 9992
2 43440 97.0588 335.6987 0003358 0.3644 359.7595 15.21553201418732Epoch: 2025-11-05T23:22Z
TLE epoch observation values (Epoch: 2025-11-05T23:22:46.433Z)
Latitude
-0.00002°
Longitude
-60.43389°
Altitude
501.947 km
Speed
7.615 km/s
True Right ascension
22h 22m 47s
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
04:49:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.413 km
Perigee altitude
495.795 km
Semi-major axis
6,876.241 km
Eccentricity
0.00034
Inclination
97.0588°
RAAN
335.6987°
Arg. of periapsis
0.3644°
True anomaly
359.75934°
Mean anomaly
359.7595°
Eccentric anomaly
359.75942°
Mean motion
3.80642 °/min
Orbital period
94.58 mins
BSTAR
0.00039178
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Other satellites on launch #40 in the year 2018 (2018-04-26 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 OVS-02 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 | 2025-11-06 14:09:04.471Z | 34.808° NE | 2025-11-06 14:12:04.471Z | 96.947° ESE | 27.57° | 2025-11-06 14:15:04.471Z | 158.87° S |
| 5 mins | 2025-11-07 02:21:04.471Z | 204.601° SW | 2025-11-07 02:23:04.471Z | 264.588° W | 32.339° | 2025-11-07 02:26:04.471Z | 330.288° 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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