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 35635U 26103.41720023 +.00000000 +00000-0 +41166-4 0 00008
2 35635 82.9537 76.3871 0020666 84.6289 25.9718 13.89945538 04
| Epoch (UTC): | 13 April 2026 10:00:46 |
| Eccentricity: | 0.0020666 |
| inclination: | 82.9537° |
| perigee height: | 914 km |
| apogee height: | 944 km |
| right ascension of ascending node: | 76.3871° |
| argument of perigee: | 84.6289° |
| revolutions per day: | 13.89945538 |
| mean anomaly at epoch: | 25.9718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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