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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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: 5 hours ago
TLE from 5 hours ago
0 NINGXIA-1 2
1 44780U 19076B 26142.58399921 -.00000084 00000-0 29818-4 0 9992
2 44780 45.0093 294.6014 0006490 23.9889 336.1246 14.02053208334268Epoch: 2026-05-22T14:00Z
TLE epoch observation values (Epoch: 2026-05-22T14:00:57.531Z)
Latitude
-0.00007°
Longitude
-155.85113°
Altitude
882.383 km
Speed
7.415 km/s
True Right ascension
19h 38m 24s
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
04:19:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
892.929 km
Perigee altitude
883.497 km
Semi-major axis
7,266.35 km
Eccentricity
0.00065
Inclination
45.0093°
RAAN
294.6014°
Arg. of periapsis
23.9889°
True anomaly
336.09448°
Mean anomaly
336.1246°
Eccentric anomaly
336.10954°
Mean motion
3.50404 °/min
Orbital period
102.74 mins
BSTAR
0.000029818
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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 | 2026-05-22 19:38:38.527Z | 288.031° WNW | 2026-05-22 19:44:38.527Z | 199.817° SSW | 38.314° | 2026-05-22 19:49:38.527Z | 139.572° SSE |
| 8 mins | 2026-05-23 12:25:38.527Z | 191.91° SSW | 2026-05-23 12:28:38.527Z | 148.106° SSE | 29.319° | 2026-05-23 12:33:38.527Z | 81.179° E |
| 10 mins | 2026-05-23 14:12:38.527Z | 251.857° W | 2026-05-23 14:16:38.527Z | 325.256° NNW | 44.67° | 2026-05-23 14:22:38.527Z | 66.409° ENE |
| 10 mins | 2026-05-23 16:00:38.527Z | 285.715° WNW | 2026-05-23 16:05:38.527Z | 13.905° NNE | 38.105° | 2026-05-23 16:10:38.527Z | 73.903° E |
| 10 mins | 2026-05-23 17:49:38.527Z | 296.648° NW | 2026-05-23 17:53:38.527Z | 6.135° NNE | 43.598° | 2026-05-23 17:59:38.527Z | 103.444° 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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