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 23080.21153934 .00001809 00000-0 23263-3 0 9995
2 44881 97.8658 160.1591 0015067 10.3344 349.8164 14.82286876175760
| Epoch (UTC): | 21 March 2023 05:04:36 |
| Eccentricity: | 0.0015067 |
| inclination: | 97.8658° |
| perigee height: | 611 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 160.1591° |
| argument of perigee: | 10.3344° |
| revolutions per day: | 14.82286876 |
| mean anomaly at epoch: | 349.8164° |
| orbit number at epoch: | 17576 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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