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 data is extracted from the following two-line orbital elements,
1 35935U 09051E 25342.67944670 .00002148 00000-0 45735-3 0 9991
2 35935 98.4167 241.5889 0008599 105.7568 254.4580 14.60020211860933
| Epoch (UTC): | 08 December 2025 16:18:24 |
| Eccentricity: | 0.0008599 |
| inclination: | 98.4167° |
| perigee height: | 687 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 241.5889° |
| argument of perigee: | 105.7568° |
| revolutions per day: | 14.60020211 |
| mean anomaly at epoch: | 254.4580° |
| orbit number at epoch: | 86093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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