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 54645U 26145.51327530 +.00000000 +00000-0 +79171-4 0 00000
2 54645 87.9252 248.5131 0002085 98.4031 261.7339 13.21825458 03
| Epoch (UTC): | 25 May 2026 12:19:06 |
| Eccentricity: | 0.0002085 |
| inclination: | 87.9252° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.5131° |
| argument of perigee: | 98.4031° |
| revolutions per day: | 13.21825458 |
| mean anomaly at epoch: | 261.7339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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