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: 22 hours ago
TLE from 22 hours ago
0 NINGXIA-1 4
1 44782U 19076D 25291.14226237 .00000049 00000-0 11664-3 0 9998
2 44782 45.0071 181.4138 0012555 55.7172 304.4849 14.01979585303855Epoch: 2025-10-18T03:24Z
TLE epoch observation values (Epoch: 2025-10-18T03:24:51.468Z)
Latitude
-0.00004°
Longitude
103.32178°
Altitude
881.792 km
Speed
7.415 km/s
True Right ascension
12h 05m 39s
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
20:36:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
897.591 km
Perigee altitude
879.344 km
Semi-major axis
7,266.604 km
Eccentricity
0.00126
Inclination
45.0071°
RAAN
181.4138°
Arg. of periapsis
55.7172°
True anomaly
304.36621°
Mean anomaly
304.4849°
Eccentric anomaly
304.42556°
Mean motion
3.50385 °/min
Orbital period
102.74 mins
BSTAR
0.00011664
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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 | 2025-10-19 02:09:07.538Z | 286.798° WNW | 2025-10-19 02:14:07.538Z | 228.115° WSW | 37.055° | 2025-10-19 02:20:07.538Z | 141.226° SSE |
| 9 mins | 2025-10-19 18:55:07.538Z | 200.721° SSW | 2025-10-19 18:59:07.538Z | 146.294° SSE | 30.711° | 2025-10-19 19:04:07.538Z | 79.581° E |
| 9 mins | 2025-10-19 20:43:07.538Z | 254.373° W | 2025-10-19 20:47:07.538Z | 342.343° N | 44.433° | 2025-10-19 20:52:07.538Z | 65.46° ENE |
| 10 mins | 2025-10-19 22:31:07.538Z | 287.066° WNW | 2025-10-19 22:35:07.538Z | 341.435° N | 37.864° | 2025-10-19 22:41:07.538Z | 75.111° E |
| 10 mins | 2025-10-20 00:20:07.538Z | 296.502° NW | 2025-10-20 00:24:07.538Z | 14.75° NNE | 43.999° | 2025-10-20 00:30:07.538Z | 105.384° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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