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 35935U 26145.49091204 +.00000000 +00000-0 +14627-3 0 00008
2 35935 98.4065 51.8816 0006585 318.1798 41.8898 14.60400249 07
| Epoch (UTC): | 25 May 2026 11:46:54 |
| Eccentricity: | 0.0006585 |
| inclination: | 98.4065° |
| perigee height: | 687 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 51.8816° |
| argument of perigee: | 318.1798° |
| revolutions per day: | 14.60400249 |
| mean anomaly at epoch: | 41.8898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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