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 37791U 26106.29913949 +.00000000 +00000-0 +46000-5 0 00006
2 37791 98.0549 198.6509 0021328 32.0686 60.8679 14.68106830 06
| Epoch (UTC): | 16 April 2026 07:10:45 |
| Eccentricity: | 0.0021328 |
| inclination: | 98.0549° |
| perigee height: | 652 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 198.6509° |
| argument of perigee: | 32.0686° |
| revolutions per day: | 14.68106830 |
| mean anomaly at epoch: | 60.8679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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