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 62294U 26145.58937259 +.00000000 +00000-0 +69158-4 0 00005
2 62294 59.9133 339.3778 0013735 357.3785 2.7148 13.75188240 03
| Epoch (UTC): | 25 May 2026 14:08:41 |
| Eccentricity: | 0.0013735 |
| inclination: | 59.9133° |
| perigee height: | 971 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 339.3778° |
| argument of perigee: | 357.3785° |
| revolutions per day: | 13.75188240 |
| mean anomaly at epoch: | 2.7148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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