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 35934U 26106.64497823 +.00000000 +00000-0 +96571-4 0 00007
2 35934 98.4077 9.2899 0007335 76.7626 283.4391 14.60094488 04
| Epoch (UTC): | 16 April 2026 15:28:46 |
| Eccentricity: | 0.0007335 |
| inclination: | 98.4077° |
| perigee height: | 688 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 9.2899° |
| argument of perigee: | 76.7626° |
| revolutions per day: | 14.60094488 |
| mean anomaly at epoch: | 283.4391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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