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 49817U 26144.63478190 +.00000000 +00000-0 +00000-0 0 00007
2 49817 0.2618 85.5364 0001739 254.8014 18.6459 1.00273134 07
| Epoch (UTC): | 24 May 2026 15:14:05 |
| Eccentricity: | 0.0001739 |
| inclination: | 0.2618° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 85.5364° |
| argument of perigee: | 254.8014° |
| revolutions per day: | 1.00273134 |
| mean anomaly at epoch: | 18.6459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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