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 35696U 26145.46106689 +.00000000 +00000-0 +00000-0 0 00000
2 35696 0.0711 91.5326 0001576 314.3183 103.6950 1.00273443 06
| Epoch (UTC): | 25 May 2026 11:03:56 |
| Eccentricity: | 0.0001576 |
| inclination: | 0.0711° |
| perigee height: | 35779 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 91.5326° |
| argument of perigee: | 314.3183° |
| revolutions per day: | 1.00273443 |
| mean anomaly at epoch: | 103.6950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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