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 data is extracted from the following two-line orbital elements,
1 11085U 78100B 22223.78945396 .00000006 00000-0 -38953-4 0 9992
2 11085 82.5480 121.2495 0012007 267.4972 158.8719 11.96552482912975
| Epoch (UTC): | 11 August 2022 18:56:48 |
| Eccentricity: | 0.0012007 |
| inclination: | 82.5480° |
| perigee height: | 1686 km |
| apogee height: | 1706 km |
| right ascension of ascending node: | 121.2495° |
| argument of perigee: | 267.4972° |
| revolutions per day: | 11.96552482 |
| mean anomaly at epoch: | 158.8719° |
| orbit number at epoch: | 91297 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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