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 35865U 26032.45344779 +.00000000 +00000-0 +73634-4 0 00003
2 35865 98.7208 356.0368 0002233 10.9641 349.1586 14.23117694 09
| Epoch (UTC): | 01 February 2026 10:52:57 |
| Eccentricity: | 0.0002233 |
| inclination: | 98.7208° |
| perigee height: | 813 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 356.0368° |
| argument of perigee: | 10.9641° |
| revolutions per day: | 14.23117694 |
| mean anomaly at epoch: | 349.1586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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