NINGXIA-1 4, 44782
Orbit data source: Space-Track
NINGXIA-1 4, 44782 is a Chinese payload satellite in LEO that was launched on Wed, 13 Nov 2019 UTC via a CHANG ZHENG 6 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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44782 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Operational Commercial Sigint
Bus & Motor
NX-1, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, Unknown HBR
Radar Cross Section
0.166 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 NINGXIA-1 4
1 44782U 19076D 25335.60877397 -.00000040 00000-0 58385-4 0 9991
2 44782 45.0097 342.7267 0014159 269.4758 90.4454 14.01992560310090Epoch: 2025-12-01T14:36Z
TLE epoch observation values (Epoch: 2025-12-01T14:36:38.071Z)
Latitude
0.00003°
Longitude
52.86227°
Altitude
886.998 km
Speed
7.41 km/s
True Right ascension
22h 50m 54s
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
03:51:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
898.711 km
Perigee altitude
878.133 km
Semi-major axis
7,266.559 km
Eccentricity
0.00142
Inclination
45.0097°
RAAN
342.7267°
Arg. of periapsis
269.4758°
True anomaly
90.60764°
Mean anomaly
90.4454°
Eccentric anomaly
90.52652°
Mean motion
3.50389 °/min
Orbital period
102.74 mins
BSTAR
0.000058385
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Other satellites on launch #76 in the year 2019 (2019-11-13 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.NINGXIA-1 4 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-12-02 06:18:30.959Z | 277.448° WNW | 2025-12-02 06:24:30.959Z | 7.083° NNE | 38.903° | 2025-12-02 06:29:30.959Z | 70.335° E |
| 10 mins | 2025-12-02 08:08:30.959Z | 296.683° NW | 2025-12-02 08:12:30.959Z | 356.716° N | 41.885° | 2025-12-02 08:18:30.959Z | 96.366° ESE |
| 10 mins | 2025-12-02 09:56:30.959Z | 284.378° WNW | 2025-12-02 10:00:30.959Z | 228.215° WSW | 38.661° | 2025-12-02 10:06:30.959Z | 138.363° SSE |
| 4 mins | 2025-12-02 11:46:30.959Z | 244.57° WSW | 2025-12-02 11:48:30.959Z | 223.523° SW | 12.897° | 2025-12-02 11:50:30.959Z | 203.572° SW |
| 9 mins | 2025-12-03 02:41:30.959Z | 196.671° SSW | 2025-12-03 02:45:30.959Z | 142.492° SSE | 29.302° | 2025-12-03 02:50:30.959Z | 80.162° E |
| 10 mins | 2025-12-03 04:28:30.959Z | 250.461° W | 2025-12-03 04:33:30.959Z | 9.903° NNE | 44.653° | 2025-12-03 04:38:30.959Z | 65.868° ENE |
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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