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 66091U 26145.33083992 +.00000000 +00000-0 +71515-3 0 00002
2 66091 53.1571 107.5299 0001155 98.5391 261.5741 15.30208732 03
| Epoch (UTC): | 25 May 2026 07:56:24 |
| Eccentricity: | 0.0001155 |
| inclination: | 53.1571° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 107.5299° |
| argument of perigee: | 98.5391° |
| revolutions per day: | 15.30208732 |
| mean anomaly at epoch: | 261.5741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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