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 59712U 26145.43200993 +.00000000 +00000-0 +14706-4 0 00007
2 59712 53.1582 308.0952 0001064 73.4968 286.6167 15.69712458 09
| Epoch (UTC): | 25 May 2026 10:22:05 |
| Eccentricity: | 0.0001064 |
| inclination: | 53.1582° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 308.0952° |
| argument of perigee: | 73.4968° |
| revolutions per day: | 15.69712458 |
| mean anomaly at epoch: | 286.6167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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