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 26110.20524605 +.00000000 +00000-0 +12241-3 0 00005
2 35935 98.4084 16.0880 0008679 62.5913 297.6169 14.60349175 09
| Epoch (UTC): | 20 April 2026 04:55:33 |
| Eccentricity: | 0.0008679 |
| inclination: | 98.4084° |
| perigee height: | 686 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 16.0880° |
| argument of perigee: | 62.5913° |
| revolutions per day: | 14.60349175 |
| mean anomaly at epoch: | 297.6169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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