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 12586U 81065B 22147.87891879 .00002987 00000-0 17677-3 0 9992
2 12586 97.6828 142.1187 0019738 123.4324 236.8797 15.12075265224953
| Epoch (UTC): | 27 May 2022 21:05:38 |
| Eccentricity: | 0.0019738 |
| inclination: | 97.6828° |
| perigee height: | 516 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 142.1187° |
| argument of perigee: | 123.4324° |
| revolutions per day: | 15.12075265 |
| mean anomaly at epoch: | 236.8797° |
| orbit number at epoch: | 22495 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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