NINGXIA-1 2, 44780
Orbit data source: Space-Track
NINGXIA-1 2, 44780 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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44780 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: 11 hours ago
TLE from 11 hours ago
0 NINGXIA-1 2
1 44780U 19076B 25312.19429781 -.00000013 00000-0 76139-4 0 9995
2 44780 45.0079 87.7140 0007455 185.5957 174.4794 14.02009233306849Epoch: 2025-11-08T04:39Z
TLE epoch observation values (Epoch: 2025-11-08T04:39:47.330Z)
Latitude
-0.00009°
Longitude
-29.8607°
Altitude
892.236 km
Speed
7.405 km/s
True Right ascension
05h 50m 51s
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
11:38:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
893.782 km
Perigee altitude
882.948 km
Semi-major axis
7,266.502 km
Eccentricity
0.00075
Inclination
45.0079°
RAAN
87.714°
Arg. of periapsis
185.5957°
True anomaly
174.48761°
Mean anomaly
174.4794°
Eccentric anomaly
174.48351°
Mean motion
3.50393 °/min
Orbital period
102.74 mins
BSTAR
0.000076139
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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 2 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 | 2025-11-08 17:03:24.974Z | 293.841° NW | 2025-11-08 17:09:24.974Z | 41.455° NE | 43.312° | 2025-11-08 17:14:24.974Z | 102.148° ESE |
| 10 mins | 2025-11-08 18:52:24.974Z | 281.854° WNW | 2025-11-08 18:57:24.974Z | 205.631° SW | 34.184° | 2025-11-08 19:02:24.974Z | 147.264° SSE |
| 9 mins | 2025-11-09 11:37:24.974Z | 207.202° SW | 2025-11-09 11:41:24.974Z | 151.819° SSE | 33.977° | 2025-11-09 11:46:24.974Z | 78.112° E |
| 10 mins | 2025-11-09 13:25:24.974Z | 259.263° W | 2025-11-09 13:29:24.974Z | 323.772° NNW | 43.562° | 2025-11-09 13:35:24.974Z | 66.246° ENE |
| 10 mins | 2025-11-09 15:13:24.974Z | 288.26° WNW | 2025-11-09 15:18:24.974Z | 9.531° NNE | 38.454° | 2025-11-09 15:23:24.974Z | 76.58° E |
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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