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 54651U 26145.52993297 +.00000000 +00000-0 -58633-3 0 00007
2 54651 87.9250 248.4916 0002117 100.9976 259.1396 13.21825578 08
| Epoch (UTC): | 25 May 2026 12:43:06 |
| Eccentricity: | 0.0002117 |
| inclination: | 87.9250° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4916° |
| argument of perigee: | 100.9976° |
| revolutions per day: | 13.21825578 |
| mean anomaly at epoch: | 259.1396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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