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 59142U 26145.40448914 +.00000000 +00000-0 +86713-3 0 00004
2 59142 97.5327 303.9986 0006975 244.4758 115.5797 15.97198519 05
| Epoch (UTC): | 25 May 2026 09:42:27 |
| Eccentricity: | 0.0006975 |
| inclination: | 97.5327° |
| perigee height: | 278 km |
| apogee height: | 287 km |
| right ascension of ascending node: | 303.9986° |
| argument of perigee: | 244.4758° |
| revolutions per day: | 15.97198519 |
| mean anomaly at epoch: | 115.5797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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