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 22138.87879389 .00004053 00000-0 23896-3 0 9990
2 12586 97.6834 133.0642 0019069 152.3866 207.8381 15.12009096223599
| Epoch (UTC): | 18 May 2022 21:05:27 |
| Eccentricity: | 0.0019069 |
| inclination: | 97.6834° |
| perigee height: | 517 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 133.0642° |
| argument of perigee: | 152.3866° |
| revolutions per day: | 15.12009096 |
| mean anomaly at epoch: | 207.8381° |
| orbit number at epoch: | 22359 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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