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 62702U 26145.62291575 +.00000000 +00000-0 +17722-3 0 00007
2 62702 97.7047 224.7243 0003178 105.5396 254.6176 14.94945881 09
| Epoch (UTC): | 25 May 2026 14:56:59 |
| Eccentricity: | 0.0003178 |
| inclination: | 97.7047° |
| perigee height: | 580 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 224.7243° |
| argument of perigee: | 105.5396° |
| revolutions per day: | 14.94945881 |
| mean anomaly at epoch: | 254.6176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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