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 35933U 26073.22844701 +.00000000 +00000-0 +23580-3 0 00003
2 35933 98.4024 339.2828 0005633 149.8471 210.3055 14.61544780 04
| Epoch (UTC): | 14 March 2026 05:28:57 |
| Eccentricity: | 0.0005633 |
| inclination: | 98.4024° |
| perigee height: | 684 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 339.2828° |
| argument of perigee: | 149.8471° |
| revolutions per day: | 14.61544780 |
| mean anomaly at epoch: | 210.3055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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