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 26103.21647513 +.00000000 +00000-0 +12241-3 0 00002
2 35935 98.4089 8.9982 0008788 81.2079 279.0115 14.60341642 05
| Epoch (UTC): | 13 April 2026 05:11:43 |
| Eccentricity: | 0.0008788 |
| inclination: | 98.4089° |
| perigee height: | 686 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 8.9982° |
| argument of perigee: | 81.2079° |
| revolutions per day: | 14.60341642 |
| mean anomaly at epoch: | 279.0115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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