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 25357.20061372 .00000182 00000-0 20317-3 0 9998
2 44782 45.0081 246.2466 0013212 8.5177 351.5879 14.01998989313128Epoch: 2025-12-23T04:48Z
TLE epoch observation values (Epoch: 2025-12-23T04:48:53.025Z)
Latitude
-0.00003°
Longitude
82.03786°
Altitude
877.387 km
Speed
7.42 km/s
True Right ascension
16h 24m 59s
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
18:47:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
898.001 km
Perigee altitude
878.8 km
Semi-major axis
7,266.537 km
Eccentricity
0.00132
Inclination
45.0081°
RAAN
246.2466°
Arg. of periapsis
8.5177°
True anomaly
351.56572°
Mean anomaly
351.5879°
Eccentric anomaly
351.57681°
Mean motion
3.5039 °/min
Orbital period
102.74 mins
BSTAR
0.00020317
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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 | 2025-12-23 20:24:02.754Z | 237.287° WSW | 2025-12-23 20:30:02.754Z | 136.635° SSE | 44.238° | 2025-12-23 20:35:02.754Z | 68.41° E |
| 10 mins | 2025-12-23 22:14:02.754Z | 279.1° WNW | 2025-12-23 22:18:02.754Z | 344.421° N | 39.54° | 2025-12-23 22:24:02.754Z | 70.068° E |
| 10 mins | 2025-12-24 00:02:02.754Z | 294.669° NW | 2025-12-24 00:07:02.754Z | 20.809° NNE | 41.045° | 2025-12-24 00:12:02.754Z | 91.128° ESE |
| 9 mins | 2025-12-24 01:51:02.754Z | 285.565° WNW | 2025-12-24 01:55:02.754Z | 210.865° SW | 41.469° | 2025-12-24 02:00:02.754Z | 133.929° SE |
| 5 mins | 2025-12-24 03:40:02.754Z | 251.821° W | 2025-12-24 03:42:02.754Z | 229.69° WSW | 15.75° | 2025-12-24 03:45:02.754Z | 196.868° SSW |
| 8 mins | 2025-12-24 18:36:02.754Z | 188.87° SSW | 2025-12-24 18:40:02.754Z | 135.577° SSE | 25.598° | 2025-12-24 18:44:02.754Z | 86.382° E |
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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