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 26072.26998940 +.00000000 +00000-0 +24453-3 0 00001
2 35933 98.4024 338.3093 0005570 152.4662 207.6835 14.61542425 09
| Epoch (UTC): | 13 March 2026 06:28:47 |
| Eccentricity: | 0.0005570 |
| inclination: | 98.4024° |
| perigee height: | 684 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 338.3093° |
| argument of perigee: | 152.4662° |
| revolutions per day: | 14.61542425 |
| mean anomaly at epoch: | 207.6835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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