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 24280.90031425 .00034746 00000-0 22842-2 0 9995
2 40024 98.0746 258.0069 0007525 133.5849 226.6003 15.07477193560057
| Epoch (UTC): | 06 October 2024 21:36:27 |
| Eccentricity: | 0.0007525 |
| inclination: | 98.0746° |
| perigee height: | 539 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 258.0069° |
| argument of perigee: | 133.5849° |
| revolutions per day: | 15.07477193 |
| mean anomaly at epoch: | 226.6003° |
| orbit number at epoch: | 56005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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