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 27560U 02054B 22222.48365327 .00000336 00000-0 82724-4 0 9998
2 27560 98.4594 26.6383 0041607 51.6534 308.8405 14.58204048 45958
| Epoch (UTC): | 10 August 2022 11:36:27 |
| Eccentricity: | 0.0041607 |
| inclination: | 98.4594° |
| perigee height: | 669 km |
| apogee height: | 728 km |
| right ascension of ascending node: | 26.6383° |
| argument of perigee: | 51.6534° |
| revolutions per day: | 14.58204048 |
| mean anomaly at epoch: | 308.8405° |
| orbit number at epoch: | 4595 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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