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 59686U 26145.55145139 +.00000000 +00000-0 -10315-4 0 00003
2 59686 43.0036 327.7170 0001139 267.3093 92.7628 15.27575492 04
| Epoch (UTC): | 25 May 2026 13:14:05 |
| Eccentricity: | 0.0001139 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.7170° |
| argument of perigee: | 267.3093° |
| revolutions per day: | 15.27575492 |
| mean anomaly at epoch: | 92.7628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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