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 59807U 26145.52119375 +.00000000 +00000-0 +30317-3 0 00000
2 59807 97.3927 217.2802 0001421 308.1561 51.9544 15.16555205 05
| Epoch (UTC): | 25 May 2026 12:30:31 |
| Eccentricity: | 0.0001421 |
| inclination: | 97.3927° |
| perigee height: | 515 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 217.2802° |
| argument of perigee: | 308.1561° |
| revolutions per day: | 15.16555205 |
| mean anomaly at epoch: | 51.9544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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