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: 14 hours ago
TLE from 14 hours ago
0 NINGXIA-1 4
1 44782U 19076D 26076.64299957 .00000024 00000-0 10012-3 0 9993
2 44782 45.0071 228.9213 0012254 50.7991 309.3929 14.02019461324974Epoch: 2026-03-17T15:25Z
TLE epoch observation values (Epoch: 2026-03-17T15:25:55.162Z)
Latitude
-0.00007°
Longitude
-177.77679°
Altitude
881.167 km
Speed
7.416 km/s
True Right ascension
15h 15m 41s
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
09:53:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
897.234 km
Perigee altitude
879.425 km
Semi-major axis
7,266.467 km
Eccentricity
0.00123
Inclination
45.0071°
RAAN
228.9213°
Arg. of periapsis
50.7991°
True anomaly
309.28428°
Mean anomaly
309.3929°
Eccentric anomaly
309.3386°
Mean motion
3.50395 °/min
Orbital period
102.74 mins
BSTAR
0.00010012
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-03-18 12:05:42.994Z | 194.879° SSW | 2026-03-18 12:10:42.994Z | 137.075° SSE | 24.961° | 2026-03-18 12:14:42.994Z | 87.476° E |
| 10 mins | 2026-03-18 13:53:42.994Z | 243.798° WSW | 2026-03-18 13:57:42.994Z | 237.865° WSW | 44.192° | 2026-03-18 14:03:42.994Z | 66.886° ENE |
| 9 mins | 2026-03-18 15:42:42.994Z | 284.85° WNW | 2026-03-18 15:46:42.994Z | 358.931° N | 38.835° | 2026-03-18 15:51:42.994Z | 70.167° E |
| 10 mins | 2026-03-18 17:30:42.994Z | 296.069° NW | 2026-03-18 17:35:42.994Z | 43.19° NE | 41.69° | 2026-03-18 17:40:42.994Z | 97.129° ESE |
| 10 mins | 2026-03-18 19:18:42.994Z | 284.358° WNW | 2026-03-18 19:23:42.994Z | 197.525° SSW | 37.687° | 2026-03-18 19:28:42.994Z | 140.155° SSE |
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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