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 22176.07438138 .00000581 00000-0 80210-4 0 9998
2 44881 97.8925 255.1738 0015563 156.5133 203.6792 14.81737769135902
| Epoch (UTC): | 25 June 2022 01:47:06 |
| Eccentricity: | 0.0015563 |
| inclination: | 97.8925° |
| perigee height: | 613 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 255.1738° |
| argument of perigee: | 156.5133° |
| revolutions per day: | 14.81737769 |
| mean anomaly at epoch: | 203.6792° |
| orbit number at epoch: | 13590 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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