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 26106.98493446 +.00000000 +00000-0 +11327-3 0 00007
2 35935 98.4087 12.8212 0008755 71.2126 289.0023 14.60345696 01
| Epoch (UTC): | 16 April 2026 23:38:18 |
| Eccentricity: | 0.0008755 |
| inclination: | 98.4087° |
| perigee height: | 686 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 12.8212° |
| argument of perigee: | 71.2126° |
| revolutions per day: | 14.60345696 |
| mean anomaly at epoch: | 289.0023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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