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 27058U 26162.19654198 +.00000000 +00000-0 +10035-3 0 00007
2 27058 82.5338 205.6739 0003337 35.8426 324.2888 12.62086833 03
| Epoch (UTC): | 11 June 2026 04:43:01 |
| Eccentricity: | 0.0003337 |
| inclination: | 82.5338° |
| perigee height: | 1412 km |
| apogee height: | 1417 km |
| right ascension of ascending node: | 205.6739° |
| argument of perigee: | 35.8426° |
| revolutions per day: | 12.62086833 |
| mean anomaly at epoch: | 324.2888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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