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 28654U 26042.21331227 +.00000000 +00000-0 +50437-4 0 00006
2 28654 98.8203 123.6853 0014946 145.9353 214.2782 14.13705165 08
| Epoch (UTC): | 11 February 2026 05:07:10 |
| Eccentricity: | 0.0014946 |
| inclination: | 98.8203° |
| perigee height: | 836 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 123.6853° |
| argument of perigee: | 145.9353° |
| revolutions per day: | 14.13705165 |
| mean anomaly at epoch: | 214.2782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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