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 59812U 26145.45059470 +.00000000 +00000-0 +12531-2 0 00004
2 59812 97.5391 252.0800 0009580 251.3780 108.6460 16.05092469 03
| Epoch (UTC): | 25 May 2026 10:48:51 |
| Eccentricity: | 0.0009580 |
| inclination: | 97.5391° |
| perigee height: | 254 km |
| apogee height: | 267 km |
| right ascension of ascending node: | 252.0800° |
| argument of perigee: | 251.3780° |
| revolutions per day: | 16.05092469 |
| mean anomaly at epoch: | 108.6460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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