View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 28371U 26145.43011949 +.00000000 +00000-0 +69131-4 0 00007
2 28371 98.5506 144.8248 0024909 9.6524 350.5147 14.56667660 09
| Epoch (UTC): | 25 May 2026 10:19:22 |
| Eccentricity: | 0.0024909 |
| inclination: | 98.5506° |
| perigee height: | 686 km |
| apogee height: | 722 km |
| right ascension of ascending node: | 144.8248° |
| argument of perigee: | 9.6524° |
| revolutions per day: | 14.56667660 |
| mean anomaly at epoch: | 350.5147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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