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 40057U 14034E 23084.18672191 .00008817 00000-0 11400-2 0 9992
2 40057 98.3725 273.4591 0010836 149.6055 210.5772 14.81126714470999
| Epoch (UTC): | 25 March 2023 04:28:52 |
| Eccentricity: | 0.0010836 |
| inclination: | 98.3725° |
| perigee height: | 618 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 273.4591° |
| argument of perigee: | 149.6055° |
| revolutions per day: | 14.81126714 |
| mean anomaly at epoch: | 210.5772° |
| orbit number at epoch: | 47099 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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