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 54663U 26145.57873830 +.00000000 +00000-0 -12236-3 0 00004
2 54663 87.9252 248.4861 0002071 98.3258 261.8111 13.21825599 02
| Epoch (UTC): | 25 May 2026 13:53:22 |
| Eccentricity: | 0.0002071 |
| inclination: | 87.9252° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4861° |
| argument of perigee: | 98.3258° |
| revolutions per day: | 13.21825599 |
| mean anomaly at epoch: | 261.8111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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