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 52257U 26145.63036524 +.00000000 +00000-0 +50613-4 0 00000
2 52257 98.1472 84.9495 0003355 348.4011 11.7110 14.57660904 03
| Epoch (UTC): | 25 May 2026 15:07:43 |
| Eccentricity: | 0.0003355 |
| inclination: | 98.1472° |
| perigee height: | 698 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 84.9495° |
| argument of perigee: | 348.4011° |
| revolutions per day: | 14.57660904 |
| mean anomaly at epoch: | 11.7110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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