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: 15 hours ago
TLE from 15 hours ago
0 NINGXIA-1 2
1 44780U 19076B 25357.30128106 -.00000106 00000-0 15648-4 0 9995
2 44780 45.0082 246.1581 0007152 28.8556 331.2673 14.02021333313179Epoch: 2025-12-23T07:13Z
TLE epoch observation values (Epoch: 2025-12-23T07:13:50.683Z)
Latitude
0.00001°
Longitude
45.60994°
Altitude
882.249 km
Speed
7.415 km/s
True Right ascension
16h 24m 37s
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
21:07:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
893.52 km
Perigee altitude
883.126 km
Semi-major axis
7,266.46 km
Eccentricity
0.00072
Inclination
45.0082°
RAAN
246.1581°
Arg. of periapsis
28.8556°
True anomaly
331.22787°
Mean anomaly
331.2673°
Eccentric anomaly
331.24759°
Mean motion
3.50396 °/min
Orbital period
102.74 mins
BSTAR
0.000015648
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-12-23 22:57:54.072Z | 285.67° WNW | 2025-12-23 23:02:54.072Z | 356.808° N | 38.448° | 2025-12-23 23:07:54.072Z | 73.925° E |
| 10 mins | 2025-12-24 00:46:54.072Z | 295.212° NW | 2025-12-24 00:51:54.072Z | 58.283° ENE | 43.849° | 2025-12-24 00:56:54.072Z | 106.268° ESE |
| 9 mins | 2025-12-24 02:34:54.072Z | 279.019° WNW | 2025-12-24 02:38:54.072Z | 228.011° WSW | 31.425° | 2025-12-24 02:43:54.072Z | 155.888° SSE |
| 9 mins | 2025-12-24 19:19:54.072Z | 211.969° SW | 2025-12-24 19:23:54.072Z | 150.319° SSE | 36.639° | 2025-12-24 19:28:54.072Z | 75.577° E |
| 10 mins | 2025-12-24 21:07:54.072Z | 263.82° W | 2025-12-24 21:11:54.072Z | 334.361° NNW | 42.803° | 2025-12-24 21:17:54.072Z | 66.631° ENE |
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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