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 56165U 26145.61243891 +.00000000 +00000-0 +74990-4 0 00001
2 56165 81.0037 93.5529 0011060 14.7217 345.4260 13.86173700 07
| Epoch (UTC): | 25 May 2026 14:41:54 |
| Eccentricity: | 0.0011060 |
| inclination: | 81.0037° |
| perigee height: | 934 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 93.5529° |
| argument of perigee: | 14.7217° |
| revolutions per day: | 13.86173700 |
| mean anomaly at epoch: | 345.4260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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