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 52458U 26145.52928708 +.00000000 +00000-0 -15906-4 0 00002
2 52458 53.2132 84.1734 0001153 89.9748 270.1377 15.08835607 04
| Epoch (UTC): | 25 May 2026 12:42:10 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 84.1734° |
| argument of perigee: | 89.9748° |
| revolutions per day: | 15.08835607 |
| mean anomaly at epoch: | 270.1377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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