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 35933U 26017.97750029 +.00000000 +00000-0 +19823-3 0 00007
2 35933 98.4073 283.1524 0005092 348.2749 11.8332 14.61380212 00
| Epoch (UTC): | 17 January 2026 23:27:36 |
| Eccentricity: | 0.0005092 |
| inclination: | 98.4073° |
| perigee height: | 685 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 283.1524° |
| argument of perigee: | 348.2749° |
| revolutions per day: | 14.61380212 |
| mean anomaly at epoch: | 11.8332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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