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 22138.51843956 -.00000014 00000-0 -29912-3 0 9991
2 11085 82.5473 169.4620 0014121 78.2587 46.0512 11.96552259902532
| Epoch (UTC): | 18 May 2022 12:26:33 |
| Eccentricity: | 0.0014121 |
| inclination: | 82.5473° |
| perigee height: | 1685 km |
| apogee height: | 1708 km |
| right ascension of ascending node: | 169.4620° |
| argument of perigee: | 78.2587° |
| revolutions per day: | 11.96552259 |
| mean anomaly at epoch: | 46.0512° |
| orbit number at epoch: | 90253 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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