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 59534U 26145.01773343 +.00000000 +00000-0 +88116-4 0 00003
2 59534 42.9986 261.5663 0000730 308.6481 51.4306 15.27574247 08
| Epoch (UTC): | 25 May 2026 00:25:32 |
| Eccentricity: | 0.0000730 |
| inclination: | 42.9986° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 261.5663° |
| argument of perigee: | 308.6481° |
| revolutions per day: | 15.27574247 |
| mean anomaly at epoch: | 51.4306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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