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 59258U 26145.38692609 +.00000000 +00000-0 +16362-4 0 00005
2 59258 53.1592 184.5760 0001069 75.2116 284.9003 15.30193082 03
| Epoch (UTC): | 25 May 2026 09:17:10 |
| Eccentricity: | 0.0001069 |
| inclination: | 53.1592° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.5760° |
| argument of perigee: | 75.2116° |
| revolutions per day: | 15.30193082 |
| mean anomaly at epoch: | 284.9003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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