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 26066.28451809 +.00000000 +00000-0 +30291-3 0 00003
2 35935 98.4118 331.5269 0007100 185.7146 174.3974 14.60262677 03
| Epoch (UTC): | 07 March 2026 06:49:42 |
| Eccentricity: | 0.0007100 |
| inclination: | 98.4118° |
| perigee height: | 687 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 331.5269° |
| argument of perigee: | 185.7146° |
| revolutions per day: | 14.60262677 |
| mean anomaly at epoch: | 174.3974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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