NINGXIA-1 5, 44783
Orbit data source: Space-Track
NINGXIA-1 5, 44783 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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44783 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: 10 hours ago
TLE from 10 hours ago
0 NINGXIA-1 5
1 44783U 19076E 25258.98861311 -.00000077 00000-0 34262-4 0 9994
2 44783 45.0068 324.4853 0011956 283.7825 76.1678 14.01961184299298Epoch: 2025-09-15T23:43Z
TLE epoch observation values (Epoch: 2025-09-15T23:43:36.172Z)
Latitude
-0.00005°
Longitude
-26.60083°
Altitude
884.945 km
Speed
7.412 km/s
True Right ascension
21h 37m 56s
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
02:23:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
897.219 km
Perigee altitude
879.843 km
Semi-major axis
7,266.668 km
Eccentricity
0.0012
Inclination
45.0068°
RAAN
324.4853°
Arg. of periapsis
283.7825°
True anomaly
76.30088°
Mean anomaly
76.1678°
Eccentric anomaly
76.23434°
Mean motion
3.50381 °/min
Orbital period
102.75 mins
BSTAR
0.000034262
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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 5 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 10:18:02.244Z | 278.986° WNW | 2025-09-16 10:24:02.244Z | 11.094° NNE | 38.558° | 2025-09-16 10:29:02.244Z | 71.41° E |
| 10 mins | 2025-09-16 12:08:02.244Z | 296.958° NW | 2025-09-16 12:12:02.244Z | 2.015° NNE | 42.45° | 2025-09-16 12:18:02.244Z | 98.339° ESE |
| 10 mins | 2025-09-16 13:56:02.244Z | 282.687° WNW | 2025-09-16 14:00:02.244Z | 222.829° SW | 37.67° | 2025-09-16 14:06:02.244Z | 140.381° SSE |
| 9 mins | 2025-09-17 06:41:02.244Z | 198.531° SSW | 2025-09-17 06:45:02.244Z | 140.707° SSE | 30.707° | 2025-09-17 06:50:02.244Z | 78.703° E |
| 10 mins | 2025-09-17 08:28:02.244Z | 252.823° W | 2025-09-17 08:33:02.244Z | 11.504° NNE | 44.313° | 2025-09-17 08:38:02.244Z | 65.723° 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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