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 35500U 26104.16259742 +.00000000 +00000-0 -46840-4 0 00002
2 35500 82.4858 127.6849 0005931 313.7420 46.3168 12.41518482 09
| Epoch (UTC): | 14 April 2026 03:54:08 |
| Eccentricity: | 0.0005931 |
| inclination: | 82.4858° |
| perigee height: | 1496 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 127.6849° |
| argument of perigee: | 313.7420° |
| revolutions per day: | 12.41518482 |
| mean anomaly at epoch: | 46.3168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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