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 59865U 26145.48088875 +.00000000 +00000-0 -40356-5 0 00006
2 59865 43.0025 204.0344 0001428 281.0029 79.0662 15.27575541 05
| Epoch (UTC): | 25 May 2026 11:32:28 |
| Eccentricity: | 0.0001428 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.0344° |
| argument of perigee: | 281.0029° |
| revolutions per day: | 15.27575541 |
| mean anomaly at epoch: | 79.0662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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