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 25350.00333770 -.00000066 00000-0 41579-4 0 9999
2 44782 45.0087 278.4042 0013758 334.6669 25.3489 14.01995932312111Epoch: 2025-12-16T00:04Z
TLE epoch observation values (Epoch: 2025-12-16T00:04:48.377Z)
Latitude
-0.00004°
Longitude
-167.6912°
Altitude
877.862 km
Speed
7.419 km/s
True Right ascension
18h 33m 36s
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
13:10:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
898.408 km
Perigee altitude
878.413 km
Semi-major axis
7,266.548 km
Eccentricity
0.00138
Inclination
45.0087°
RAAN
278.4042°
Arg. of periapsis
334.6669°
True anomaly
25.4165°
Mean anomaly
25.3489°
Eccentric anomaly
25.38269°
Mean motion
3.50389 °/min
Orbital period
102.74 mins
BSTAR
0.000041579
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-16 20:44:48.679Z | 165.179° S | 2025-12-16 20:47:48.679Z | 133.624° SE | 15.095° | 2025-12-16 20:50:48.679Z | 101.792° ESE |
| 10 mins | 2025-12-16 22:30:48.679Z | 223.017° SW | 2025-12-16 22:34:48.679Z | 162.098° S | 40.839° | 2025-12-16 22:40:48.679Z | 70.349° E |
| 10 mins | 2025-12-17 00:18:48.679Z | 270.355° WNW | 2025-12-17 00:22:48.679Z | 326.442° NNW | 40.819° | 2025-12-17 00:28:48.679Z | 67.098° ENE |
| 10 mins | 2025-12-17 02:07:48.679Z | 295.598° NW | 2025-12-17 02:11:48.679Z | 4.379° NNE | 39.562° | 2025-12-17 02:17:48.679Z | 85.917° E |
| 10 mins | 2025-12-17 03:55:48.679Z | 291.191° WNW | 2025-12-17 03:59:48.679Z | 253.082° W | 43.907° | 2025-12-17 04:05:48.679Z | 122.038° SE |
| 7 mins | 2025-12-17 05:44:48.679Z | 260.489° W | 2025-12-17 05:47:48.679Z | 222.021° SW | 21.742° | 2025-12-17 05:51:48.679Z | 176.436° S |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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