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 26069.64205315 +.00000000 +00000-0 +25245-3 0 00008
2 35935 98.4112 334.9339 0007329 175.0903 185.0370 14.60270533 07
| Epoch (UTC): | 10 March 2026 15:24:33 |
| Eccentricity: | 0.0007329 |
| inclination: | 98.4112° |
| perigee height: | 687 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 334.9339° |
| argument of perigee: | 175.0903° |
| revolutions per day: | 14.60270533 |
| mean anomaly at epoch: | 185.0370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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