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 40024U 14033Q 24357.52940219 .00018514 00000-0 11031-2 0 9991
2 40024 98.0821 338.7140 0002955 254.7262 105.3640 15.11245915571618
| Epoch (UTC): | 22 December 2024 12:42:20 |
| Eccentricity: | 0.0002955 |
| inclination: | 98.0821° |
| perigee height: | 530 km |
| apogee height: | 534 km |
| right ascension of ascending node: | 338.7140° |
| argument of perigee: | 254.7262° |
| revolutions per day: | 15.11245915 |
| mean anomaly at epoch: | 105.3640° |
| orbit number at epoch: | 57161 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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