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 54975U 26017.26122600 +.00000000 +00000-0 +44806-2 0 00002
2 54975 98.8203 132.2396 0059141 319.5178 40.1654 15.09760712 00
| Epoch (UTC): | 17 January 2026 06:16:09 |
| Eccentricity: | 0.0059141 |
| inclination: | 98.8203° |
| perigee height: | 496 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 132.2396° |
| argument of perigee: | 319.5178° |
| revolutions per day: | 15.09760712 |
| mean anomaly at epoch: | 40.1654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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