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 59700U 26145.60175554 +.00000000 +00000-0 +22681-4 0 00008
2 59700 43.0031 345.6396 0000725 273.7049 86.3719 15.27575981 00
| Epoch (UTC): | 25 May 2026 14:26:31 |
| Eccentricity: | 0.0000725 |
| inclination: | 43.0031° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.6396° |
| argument of perigee: | 273.7049° |
| revolutions per day: | 15.27575981 |
| mean anomaly at epoch: | 86.3719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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