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 54658U 26145.52827784 +.00000000 +00000-0 +31195-3 0 00004
2 54658 87.9261 248.4708 0001994 100.5391 259.5968 13.21825174 06
| Epoch (UTC): | 25 May 2026 12:40:43 |
| Eccentricity: | 0.0001994 |
| inclination: | 87.9261° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4708° |
| argument of perigee: | 100.5391° |
| revolutions per day: | 13.21825174 |
| mean anomaly at epoch: | 259.5968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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