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 59862U 26145.55655824 +.00000000 +00000-0 +44677-5 0 00004
2 59862 43.0036 203.7547 0001598 273.6339 86.4330 15.27571001 05
| Epoch (UTC): | 25 May 2026 13:21:26 |
| Eccentricity: | 0.0001598 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 203.7547° |
| argument of perigee: | 273.6339° |
| revolutions per day: | 15.27571001 |
| mean anomaly at epoch: | 86.4330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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