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 52859U 26145.11846468 +.00000000 +00000-0 +36358-4 0 00007
2 52859 53.2138 41.0152 0001312 87.5657 272.5485 15.08840070 07
| Epoch (UTC): | 25 May 2026 02:50:35 |
| Eccentricity: | 0.0001312 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 41.0152° |
| argument of perigee: | 87.5657° |
| revolutions per day: | 15.08840070 |
| mean anomaly at epoch: | 272.5485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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