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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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: 14 hours ago
TLE from 14 hours ago
0 NINGXIA-1 4
1 44782U 19076D 25325.70360521 -.00000045 00000-0 54784-4 0 9991
2 44782 45.0099 26.9845 0013888 224.8190 135.1523 14.01990769308706Epoch: 2025-11-21T16:53Z
TLE epoch observation values (Epoch: 2025-11-21T16:53:11.490Z)
Latitude
0°
Longitude
72.74381°
Altitude
894.069 km
Speed
7.403 km/s
True Right ascension
01h 47m 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
04:25:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
898.52 km
Perigee altitude
878.336 km
Semi-major axis
7,266.565 km
Eccentricity
0.00139
Inclination
45.0099°
RAAN
26.9845°
Arg. of periapsis
224.819°
True anomaly
135.26439°
Mean anomaly
135.1523°
Eccentric anomaly
135.20836°
Mean motion
3.50388 °/min
Orbital period
102.74 mins
BSTAR
0.000054784
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-22 08:31:02.668Z | 252.683° W | 2025-11-22 08:36:02.668Z | 310.503° NW | 44.304° | 2025-11-22 08:42:02.668Z | 66.198° ENE |
| 10 mins | 2025-11-22 10:20:02.668Z | 286.021° WNW | 2025-11-22 10:25:02.668Z | 7.62° NNE | 38.466° | 2025-11-22 10:30:02.668Z | 74.141° E |
| 10 mins | 2025-11-22 12:09:02.668Z | 295.952° NW | 2025-11-22 12:13:02.668Z | 347.748° N | 43.655° | 2025-11-22 12:19:02.668Z | 104.983° ESE |
| 9 mins | 2025-11-22 13:57:02.668Z | 278.489° WNW | 2025-11-22 14:01:02.668Z | 222.187° SW | 32.811° | 2025-11-22 14:06:02.668Z | 152.662° SSE |
| 10 mins | 2025-11-23 06:41:02.668Z | 212.918° SW | 2025-11-23 06:46:02.668Z | 140.858° SSE | 35.81° | 2025-11-23 06:51:02.668Z | 75.298° E |
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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