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 55660U 26145.49684045 +.00000000 +00000-0 +15005-4 0 00008
2 55660 69.9988 330.6388 0002573 270.6095 89.4769 14.98328441 07
| Epoch (UTC): | 25 May 2026 11:55:27 |
| Eccentricity: | 0.0002573 |
| inclination: | 69.9988° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.6388° |
| argument of perigee: | 270.6095° |
| revolutions per day: | 14.98328441 |
| mean anomaly at epoch: | 89.4769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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