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 26072.79400777 +.00000000 +00000-0 +23882-3 0 00002
2 35935 98.4112 338.1321 0007540 165.3239 194.8181 14.60278143 06
| Epoch (UTC): | 13 March 2026 19:03:22 |
| Eccentricity: | 0.0007540 |
| inclination: | 98.4112° |
| perigee height: | 687 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 338.1321° |
| argument of perigee: | 165.3239° |
| revolutions per day: | 14.60278143 |
| mean anomaly at epoch: | 194.8181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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