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: 10 hours ago
TLE from 10 hours ago
0 NINGXIA-1 1
1 44779U 19076A 25258.97619208 -.00000051 00000-0 50967-4 0 9996
2 44779 45.0070 325.1998 0011942 294.3496 65.6091 14.01975822299376Epoch: 2025-09-15T23:25Z
TLE epoch observation values (Epoch: 2025-09-15T23:25:42.995Z)
Latitude
-0.00003°
Longitude
-21.4025°
Altitude
883.387 km
Speed
7.414 km/s
True Right ascension
21h 40m 47s
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
02:22:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
897.158 km
Perigee altitude
879.803 km
Semi-major axis
7,266.617 km
Eccentricity
0.00119
Inclination
45.007°
RAAN
325.1998°
Arg. of periapsis
294.3496°
True anomaly
65.73381°
Mean anomaly
65.6091°
Eccentric anomaly
65.67145°
Mean motion
3.50384 °/min
Orbital period
102.74 mins
BSTAR
0.000050967
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-09-16 09:58:57.698Z | 273.679° WNW | 2025-09-16 10:04:57.698Z | 9.798° NNE | 39.39° | 2025-09-16 10:09:57.698Z | 68.737° E |
| 10 mins | 2025-09-16 11:48:57.698Z | 296.616° NW | 2025-09-16 11:52:57.698Z | 1.483° NNE | 40.849° | 2025-09-16 11:58:57.698Z | 91.697° ESE |
| 10 mins | 2025-09-16 13:36:57.698Z | 287.43° WNW | 2025-09-16 13:40:57.698Z | 233.01° WSW | 41.513° | 2025-09-16 13:46:57.698Z | 131.481° SE |
| 6 mins | 2025-09-16 15:25:57.698Z | 256.315° W | 2025-09-16 15:28:57.698Z | 222.749° SW | 16.435° | 2025-09-16 15:31:57.698Z | 191.135° SSW |
| 8 mins | 2025-09-17 06:22:57.698Z | 182.452° SSW | 2025-09-17 06:25:57.698Z | 142.032° SSE | 25.046° | 2025-09-17 06:30:57.698Z | 83.194° E |
| 10 mins | 2025-09-17 08:08:57.698Z | 243.62° WSW | 2025-09-17 08:13:57.698Z | 85.709° E | 44.859° | 2025-09-17 08:18:57.698Z | 66.9° ENE |
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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