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 57166U 26156.85649992 +.00000000 +00000-0 +20643-4 0 00009
2 57166 98.6086 212.0661 0003695 186.2105 173.9029 14.24045844 05
| Epoch (UTC): | 05 June 2026 20:33:21 |
| Eccentricity: | 0.0003695 |
| inclination: | 98.6086° |
| perigee height: | 809 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 212.0661° |
| argument of perigee: | 186.2105° |
| revolutions per day: | 14.24045844 |
| mean anomaly at epoch: | 173.9029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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