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 06080U 26066.20380894 +.00000000 +00000-0 +19198-4 0 00003
2 06080 81.2421 170.7995 0048502 350.9513 9.0774 14.01289777 00
| Epoch (UTC): | 07 March 2026 04:53:29 |
| Eccentricity: | 0.0048502 |
| inclination: | 81.2421° |
| perigee height: | 854 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 170.7995° |
| argument of perigee: | 350.9513° |
| revolutions per day: | 14.01289777 |
| mean anomaly at epoch: | 9.0774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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