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 26497U 00054D 24357.78045138 .00000180 00000-0 32484-2 0 9996
2 26497 7.5538 356.1931 7140102 17.4854 219.1871 2.27881395201344
| Epoch (UTC): | 22 December 2024 18:43:50 |
| Eccentricity: | 0.7140102 |
| inclination: | 7.5538° |
| perigee height: | 598 km |
| apogee height: | 35431 km |
| right ascension of ascending node: | 356.1931° |
| argument of perigee: | 17.4854° |
| revolutions per day: | 2.27881395 |
| mean anomaly at epoch: | 219.1871° |
| orbit number at epoch: | 20134 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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