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 55640U 26145.00472807 +.00000000 +00000-0 -53603-4 0 00001
2 55640 69.9996 351.9981 0002260 263.6551 96.4351 14.98335464 09
| Epoch (UTC): | 25 May 2026 00:06:48 |
| Eccentricity: | 0.0002260 |
| inclination: | 69.9996° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 351.9981° |
| argument of perigee: | 263.6551° |
| revolutions per day: | 14.98335464 |
| mean anomaly at epoch: | 96.4351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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