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 27945U 03042G 23083.64458020 .00001501 00000-0 28613-3 0 9991
2 27945 98.2263 220.9108 0013192 87.7264 272.5449 14.65446548 41444
| Epoch (UTC): | 24 March 2023 15:28:11 |
| Eccentricity: | 0.0013192 |
| inclination: | 98.2263° |
| perigee height: | 666 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 220.9108° |
| argument of perigee: | 87.7264° |
| revolutions per day: | 14.65446548 |
| mean anomaly at epoch: | 272.5449° |
| orbit number at epoch: | 4144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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