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 38157U 99025ERE 24357.58870371 .00003839 00000-0 12504-2 0 9996
2 38157 99.6893 224.9520 0282969 29.7438 331.9490 14.19047468712051
| Epoch (UTC): | 22 December 2024 14:07:44 |
| Eccentricity: | 0.0282969 |
| inclination: | 99.6893° |
| perigee height: | 624 km |
| apogee height: | 1032 km |
| right ascension of ascending node: | 224.9520° |
| argument of perigee: | 29.7438° |
| revolutions per day: | 14.19047468 |
| mean anomaly at epoch: | 331.9490° |
| orbit number at epoch: | 71205 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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