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 38547U 91032G 24357.18705546 .00000715 00000-0 29172-3 0 9996
2 38547 98.4736 343.9945 0005602 135.3128 224.8507 14.30344469685712
| Epoch (UTC): | 22 December 2024 04:29:21 |
| Eccentricity: | 0.0005602 |
| inclination: | 98.4736° |
| perigee height: | 786 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 343.9945° |
| argument of perigee: | 135.3128° |
| revolutions per day: | 14.30344469 |
| mean anomaly at epoch: | 224.8507° |
| orbit number at epoch: | 68571 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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