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 68710U 26145.59799549 +.00000000 +00000-0 -64529-3 0 00000
2 68710 53.1591 37.1636 0001063 198.0635 162.0335 15.47101748 04
| Epoch (UTC): | 25 May 2026 14:21:06 |
| Eccentricity: | 0.0001063 |
| inclination: | 53.1591° |
| perigee height: | 424 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 37.1636° |
| argument of perigee: | 198.0635° |
| revolutions per day: | 15.47101748 |
| mean anomaly at epoch: | 162.0335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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