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 25349.25853238 .00001101 00000-0 23938-3 0 9990
2 35935 98.4165 248.2673 0008746 88.3693 271.8508 14.60038836861896
| Epoch (UTC): | 15 December 2025 06:12:17 |
| Eccentricity: | 0.0008746 |
| inclination: | 98.4165° |
| perigee height: | 687 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 248.2673° |
| argument of perigee: | 88.3693° |
| revolutions per day: | 14.60038836 |
| mean anomaly at epoch: | 271.8508° |
| orbit number at epoch: | 86189 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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