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 54660U 26145.57031782 +.00000000 +00000-0 -53694-4 0 00007
2 54660 87.9252 248.4925 0001886 100.7679 259.3667 13.21827765 03
| Epoch (UTC): | 25 May 2026 13:41:15 |
| Eccentricity: | 0.0001886 |
| inclination: | 87.9252° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4925° |
| argument of perigee: | 100.7679° |
| revolutions per day: | 13.21827765 |
| mean anomaly at epoch: | 259.3667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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