NAXING 1, 28221
Orbit data source: Space-Track
NAXING 1, 28221 is a payload satellite owned by CASC (CN) in SSO that was launched on Sun, 18 Apr 2004 UTC via a CHANG ZHENG 2C launch vehicle from the Xichang Space Center, China (XSC). 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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28221 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Tsinghua
Mission
Civil Technology
Bus & Motor
NX, Unknown motor
Mass
25 kg wet, 25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.060 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 NAXING 1
1 28221U 04012B 26034.50607866 .00002221 00000-0 16009-3 0 9991
2 28221 98.0168 57.1678 0011056 173.1232 187.0147 15.05234848187133Epoch: 2026-02-03T12:08Z
TLE epoch observation values (Epoch: 2026-02-03T12:08:45.196Z)
Latitude
-0.00001°
Longitude
101.29345°
Altitude
561.442 km
Speed
7.576 km/s
True Right ascension
03h 48m 40s
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
07:07:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
555.455 km
Perigee altitude
540.14 km
Semi-major axis
6,925.934 km
Eccentricity
0.00111
Inclination
98.0168°
RAAN
57.1678°
Arg. of periapsis
173.1232°
True anomaly
186.99925°
Mean anomaly
187.0147°
Eccentric anomaly
187.00697°
Mean motion
3.76553 °/min
Orbital period
95.6 mins
BSTAR
0.00016009
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Other satellites on launch #12 in the year 2004 (2004-04-18 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.NAXING 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-04 14:13:55.564Z | 15.238° NNE | 2026-02-04 14:17:55.564Z | 166.542° S | 42.939° | 2026-02-04 14:20:55.564Z | 189.785° SSW |
| 6 mins | 2026-02-05 00:58:55.564Z | 135.935° SSE | 2026-02-05 01:01:55.564Z | 55.093° ENE | 32.925° | 2026-02-05 01:04:55.564Z | 3.458° NNE |
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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