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 37613U 26085.46440626 +.00000000 +00000-0 +24427-2 0 00007
2 37613 98.8517 273.0598 0149193 280.9116 77.5299 14.09961113 02
| Epoch (UTC): | 26 March 2026 11:08:44 |
| Eccentricity: | 0.0149193 |
| inclination: | 98.8517° |
| perigee height: | 752 km |
| apogee height: | 967 km |
| right ascension of ascending node: | 273.0598° |
| argument of perigee: | 280.9116° |
| revolutions per day: | 14.09961113 |
| mean anomaly at epoch: | 77.5299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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