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 55288U 26145.42445575 +.00000000 +00000-0 +30049-4 0 00005
2 55288 69.9986 190.9635 0003695 267.0904 92.9832 14.98332161 02
| Epoch (UTC): | 25 May 2026 10:11:12 |
| Eccentricity: | 0.0003695 |
| inclination: | 69.9986° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.9635° |
| argument of perigee: | 267.0904° |
| revolutions per day: | 14.98332161 |
| mean anomaly at epoch: | 92.9832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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