NINGXIA-1 4, 44782
Orbit data source: Space-Track
NINGXIA-1 4, 44782 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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44782 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: 9 hours ago
TLE from 9 hours ago
0 NINGXIA-1 4
1 44782U 19076D 26166.92517704 .00000097 00000-0 14777-3 0 9999
2 44782 45.0062 185.4669 0011624 120.8505 239.3474 14.02070236337648Epoch: 2026-06-15T22:12Z
TLE epoch observation values (Epoch: 2026-06-15T22:12:15.296Z)
Latitude
-0.00001°
Longitude
-51.80141°
Altitude
890.947 km
Speed
7.406 km/s
True Right ascension
12h 21m 52s
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
17:26:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
896.601 km
Perigee altitude
879.708 km
Semi-major axis
7,266.291 km
Eccentricity
0.00116
Inclination
45.0062°
RAAN
185.4669°
Arg. of periapsis
120.8505°
True anomaly
239.2329°
Mean anomaly
239.3474°
Eccentric anomaly
239.29014°
Mean motion
3.50408 °/min
Orbital period
102.74 mins
BSTAR
0.00014777
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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 4 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 | 2026-06-16 07:04:13.701Z | 279.392° WNW | 2026-06-16 07:09:13.701Z | 348.955° N | 38.868° | 2026-06-16 07:14:13.701Z | 69.109° E |
| 10 mins | 2026-06-16 08:53:13.701Z | 295.384° NW | 2026-06-16 08:58:13.701Z | 29.337° NE | 42.064° | 2026-06-16 09:03:13.701Z | 96.156° ESE |
| 9 mins | 2026-06-16 10:42:13.701Z | 281.315° WNW | 2026-06-16 10:46:13.701Z | 205.696° SW | 38.321° | 2026-06-16 10:51:13.701Z | 140.191° SSE |
| 8 mins | 2026-06-17 03:27:13.701Z | 193.507° SSW | 2026-06-17 03:31:13.701Z | 130.802° SE | 29.311° | 2026-06-17 03:35:13.701Z | 82.054° E |
| 10 mins | 2026-06-17 05:14:13.701Z | 251.852° W | 2026-06-17 05:18:13.701Z | 300.696° NW | 44.473° | 2026-06-17 05:24:13.701Z | 66.285° 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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