NINGXIA-1 6, 49018
Orbit data source: Space-Track
NINGXIA-1 6, 49018 is a Chinese payload satellite in LEO that was launched on Fri, 09 Jul 2021 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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49018 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, 0.5 m
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 6
1 49018U 21064A 26171.53706118 .00000093 00000-0 12975-3 0 9992
2 49018 44.9984 211.9650 0009239 248.3201 111.6652 14.08535727254688Epoch: 2026-06-20T12:53Z
TLE epoch observation values (Epoch: 2026-06-20T12:53:22.085Z)
Latitude
-0.00003°
Longitude
109.87268°
Altitude
866.861 km
Speed
7.419 km/s
True Right ascension
14h 07m 51s
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
14:08:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
872.605 km
Perigee altitude
859.219 km
Semi-major axis
7,244.049 km
Eccentricity
0.00092
Inclination
44.9984°
RAAN
211.965°
Arg. of periapsis
248.3201°
True anomaly
111.76355°
Mean anomaly
111.6652°
Eccentric anomaly
111.71438°
Mean motion
3.52023 °/min
Orbital period
102.27 mins
BSTAR
0.00012975
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Other satellites on launch #64 in the year 2021 (2021-07-09 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 6 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-21 04:20:52.674Z | 176.95° S | 2026-06-21 04:24:52.674Z | 133.623° SE | 17.862° | 2026-06-21 04:27:52.674Z | 99.355° ESE |
| 10 mins | 2026-06-21 06:06:52.674Z | 230.577° WSW | 2026-06-21 06:11:52.674Z | 132.861° SE | 42.788° | 2026-06-21 06:16:52.674Z | 69.676° E |
| 10 mins | 2026-06-21 07:54:52.674Z | 274.12° WNW | 2026-06-21 07:58:52.674Z | 329.167° NNW | 39.749° | 2026-06-21 08:04:52.674Z | 68.07° E |
| 10 mins | 2026-06-21 09:42:52.674Z | 294.446° NW | 2026-06-21 09:47:52.674Z | 27.208° NE | 39.687° | 2026-06-21 09:52:52.674Z | 87.883° E |
| 10 mins | 2026-06-21 11:30:52.674Z | 289.201° WNW | 2026-06-21 11:34:52.674Z | 234.367° WSW | 43.009° | 2026-06-21 11:40:52.674Z | 126.693° SE |
| 6 mins | 2026-06-21 13:19:52.674Z | 252.221° W | 2026-06-21 13:21:52.674Z | 227.451° WSW | 18.499° | 2026-06-21 13:25:52.674Z | 182.663° SSW |
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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