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 56716U 26145.31128271 +.00000000 +00000-0 +16951-3 0 00006
2 56716 87.9262 248.5206 0002396 112.0037 248.1351 13.21823916 02
| Epoch (UTC): | 25 May 2026 07:28:14 |
| Eccentricity: | 0.0002396 |
| inclination: | 87.9262° |
| perigee height: | 1176 km |
| apogee height: | 1180 km |
| right ascension of ascending node: | 248.5206° |
| argument of perigee: | 112.0037° |
| revolutions per day: | 13.21823916 |
| mean anomaly at epoch: | 248.1351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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