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 09040U 75004DE 24262.49642610 .00000961 00000-0 26499-3 0 9996
2 09040 97.9862 355.2486 0047494 137.2457 223.2448 14.48210079521184
| Epoch (UTC): | 18 September 2024 11:54:51 |
| Eccentricity: | 0.0047494 |
| inclination: | 97.9862° |
| perigee height: | 698 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 355.2486° |
| argument of perigee: | 137.2457° |
| revolutions per day: | 14.48210079 |
| mean anomaly at epoch: | 223.2448° |
| orbit number at epoch: | 52118 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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