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 44881U 19093C 22175.87179223 .00000589 00000-0 81281-4 0 9999
2 44881 97.8925 254.9741 0015520 157.1643 203.0251 14.81737584135874
| Epoch (UTC): | 24 June 2022 20:55:22 |
| Eccentricity: | 0.0015520 |
| inclination: | 97.8925° |
| perigee height: | 613 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 254.9741° |
| argument of perigee: | 157.1643° |
| revolutions per day: | 14.81737584 |
| mean anomaly at epoch: | 203.0251° |
| orbit number at epoch: | 13587 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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