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 52860U 26145.12582501 +.00000000 +00000-0 -10049-3 0 00004
2 52860 53.2130 40.9845 0001854 86.9591 273.1613 15.08847402 05
| Epoch (UTC): | 25 May 2026 03:01:11 |
| Eccentricity: | 0.0001854 |
| inclination: | 53.2130° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 40.9845° |
| argument of perigee: | 86.9591° |
| revolutions per day: | 15.08847402 |
| mean anomaly at epoch: | 273.1613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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