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 26108.56083245 +.00000000 +00000-0 +12965-3 0 00004
2 35935 98.4085 14.4198 0008719 67.0056 293.2063 14.60347710 05
| Epoch (UTC): | 18 April 2026 13:27:35 |
| Eccentricity: | 0.0008719 |
| inclination: | 98.4085° |
| perigee height: | 686 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 14.4198° |
| argument of perigee: | 67.0056° |
| revolutions per day: | 14.60347710 |
| mean anomaly at epoch: | 293.2063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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