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 56060U 26145.57200145 +.00000000 +00000-0 +27125-5 0 00004
2 56060 87.9256 248.4726 0001755 99.9138 260.2194 13.21826178 09
| Epoch (UTC): | 25 May 2026 13:43:40 |
| Eccentricity: | 0.0001755 |
| inclination: | 87.9256° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4726° |
| argument of perigee: | 99.9138° |
| revolutions per day: | 13.21826178 |
| mean anomaly at epoch: | 260.2194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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