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 26145.17756527 +.00000000 +00000-0 +15561-3 0 00005
2 35933 98.3981 52.3476 0004240 310.2632 49.8197 14.61676163 06
| Epoch (UTC): | 25 May 2026 04:15:41 |
| Eccentricity: | 0.0004240 |
| inclination: | 98.3981° |
| perigee height: | 685 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 52.3476° |
| argument of perigee: | 310.2632° |
| revolutions per day: | 14.61676163 |
| mean anomaly at epoch: | 49.8197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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