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 40462U 95015BE 24355.48963784 .00015319 00000-0 56610-2 0 9993
2 40462 98.9651 6.1762 0039747 173.6075 186.5622 14.32032585503525
| Epoch (UTC): | 20 December 2024 11:45:04 |
| Eccentricity: | 0.0039747 |
| inclination: | 98.9651° |
| perigee height: | 756 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 6.1762° |
| argument of perigee: | 173.6075° |
| revolutions per day: | 14.32032585 |
| mean anomaly at epoch: | 186.5622° |
| orbit number at epoch: | 50352 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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