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 23159.55907360 .00003650 00000-0 46856-3 0 9999
2 40057 98.3723 352.2076 0008704 269.9646 90.0568 14.81856779482150
| Epoch (UTC): | 08 June 2023 13:25:03 |
| Eccentricity: | 0.0008704 |
| inclination: | 98.3723° |
| perigee height: | 617 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 352.2076° |
| argument of perigee: | 269.9646° |
| revolutions per day: | 14.81856779 |
| mean anomaly at epoch: | 90.0568° |
| orbit number at epoch: | 48215 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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