NINGXIA-1 1, 44779
Orbit data source: Space-Track
NINGXIA-1 1, 44779 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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44779 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 NINGXIA-1 1
1 44779U 19076A 25312.49296661 -.00000011 00000-0 76998-4 0 9996
2 44779 45.0063 86.0603 0011695 194.0037 166.0474 14.01992333306888Epoch: 2025-11-08T11:49Z
TLE epoch observation values (Epoch: 2025-11-08T11:49:52.315Z)
Latitude
-0.00001°
Longitude
-139.32948°
Altitude
895.149 km
Speed
7.402 km/s
True Right ascension
05h 44m 14s
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
14:38:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
896.922 km
Perigee altitude
879.925 km
Semi-major axis
7,266.56 km
Eccentricity
0.00117
Inclination
45.0063°
RAAN
86.0603°
Arg. of periapsis
194.0037°
True anomaly
166.07967°
Mean anomaly
166.0474°
Eccentric anomaly
166.06354°
Mean motion
3.50388 °/min
Orbital period
102.74 mins
BSTAR
0.000076998
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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 1 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 | 2025-11-08 19:12:43.436Z | 279.732° WNW | 2025-11-08 19:17:43.436Z | 217.841° SW | 28.76° | 2025-11-08 19:22:43.436Z | 158.201° S |
| 4 mins | 2025-11-09 10:13:43.436Z | 147.685° SSE | 2025-11-09 10:14:43.436Z | 137.215° SSE | 13.178° | 2025-11-09 10:17:43.436Z | 106.388° ESE |
| 10 mins | 2025-11-09 11:57:43.436Z | 219.497° SW | 2025-11-09 12:02:43.436Z | 133.795° SE | 39.009° | 2025-11-09 12:07:43.436Z | 72.388° E |
| 10 mins | 2025-11-09 13:45:43.436Z | 266.184° W | 2025-11-09 13:50:43.436Z | 359.855° N | 41.856° | 2025-11-09 13:55:43.436Z | 65.865° ENE |
| 10 mins | 2025-11-09 15:34:43.436Z | 293.181° NW | 2025-11-09 15:38:43.436Z | 351.04° N | 38.789° | 2025-11-09 15:44:43.436Z | 82.771° E |
| 10 mins | 2025-11-09 17:22:43.436Z | 292.645° NW | 2025-11-09 17:27:43.436Z | 154.398° SSE | 44.744° | 2025-11-09 17:32:43.436Z | 118.193° SE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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