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 40468U 95015BL 24280.30831084 .00019080 00000-0 69065-2 0 9991
2 40468 98.6745 307.1868 0007979 273.5109 86.5162 14.33437571499205
| Epoch (UTC): | 06 October 2024 07:23:58 |
| Eccentricity: | 0.0007979 |
| inclination: | 98.6745° |
| perigee height: | 774 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 307.1868° |
| argument of perigee: | 273.5109° |
| revolutions per day: | 14.33437571 |
| mean anomaly at epoch: | 86.5162° |
| orbit number at epoch: | 49920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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