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 40681U 95015FV 24358.01723023 .00009250 00000-0 35105-2 0 9991
2 40681 98.7415 17.9627 0005115 216.9986 143.0844 14.31257844503113
| Epoch (UTC): | 23 December 2024 00:24:48 |
| Eccentricity: | 0.0005115 |
| inclination: | 98.7415° |
| perigee height: | 784 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 17.9627° |
| argument of perigee: | 216.9986° |
| revolutions per day: | 14.31257844 |
| mean anomaly at epoch: | 143.0844° |
| orbit number at epoch: | 50311 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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