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 26075.19222403 +.00000000 +00000-0 +20305-3 0 00004
2 35935 98.4111 340.5657 0007715 157.9119 202.2414 14.60282734 06
| Epoch (UTC): | 16 March 2026 04:36:48 |
| Eccentricity: | 0.0007715 |
| inclination: | 98.4111° |
| perigee height: | 687 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 340.5657° |
| argument of perigee: | 157.9119° |
| revolutions per day: | 14.60282734 |
| mean anomaly at epoch: | 202.2414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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