NINGXIA-1 1, 44779
Orbit data source: Space-Track
NINGXIA-1 1, 44779 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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44779 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 NINGXIA-1 1
1 44779U 19076A 25357.31545981 .00000004 00000-0 86926-4 0 9991
2 44779 45.0050 245.7749 0011160 40.4259 319.7403 14.02005166313175Epoch: 2025-12-23T07:34Z
TLE epoch observation values (Epoch: 2025-12-23T07:34:15.727Z)
Latitude
0.00001°
Longitude
40.10841°
Altitude
880.677 km
Speed
7.417 km/s
True Right ascension
16h 23m 05s
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
21:06:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
896.489 km
Perigee altitude
880.27 km
Semi-major axis
7,266.516 km
Eccentricity
0.00112
Inclination
45.005°
RAAN
245.7749°
Arg. of periapsis
40.4259°
True anomaly
319.65757°
Mean anomaly
319.7403°
Eccentric anomaly
319.69894°
Mean motion
3.50392 °/min
Orbital period
102.74 mins
BSTAR
0.000086926
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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 1 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 | 2025-12-23 23:19:06.048Z | 287.984° WNW | 2025-12-23 23:25:06.048Z | 20.227° NNE | 38.404° | 2025-12-23 23:30:06.048Z | 80.498° E |
| 10 mins | 2025-12-24 01:09:06.048Z | 293.506° NW | 2025-12-24 01:13:06.048Z | 260.188° W | 45° | 2025-12-24 01:19:06.048Z | 115.25° SE |
| 8 mins | 2025-12-24 02:57:06.048Z | 269.434° W | 2025-12-24 03:01:06.048Z | 214.414° SW | 25.64° | 2025-12-24 03:05:06.048Z | 167.293° S |
| 5 mins | 2025-12-24 17:56:06.048Z | 158.071° S | 2025-12-24 17:58:06.048Z | 135.763° SSE | 15.488° | 2025-12-24 18:01:06.048Z | 102.974° ESE |
| 10 mins | 2025-12-24 19:41:06.048Z | 224.665° SW | 2025-12-24 19:45:06.048Z | 171.073° S | 40.849° | 2025-12-24 19:51:06.048Z | 70.401° E |
| 10 mins | 2025-12-24 21:29:06.048Z | 270.48° WNW | 2025-12-24 21:34:06.048Z | 7.006° NNE | 40.646° | 2025-12-24 21:39:06.048Z | 66.892° ENE |
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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