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 54397U 22151DV 24279.84869967 .00054468 00000-0 72263-2 0 9999
2 54397 98.5180 317.8966 0118526 257.1647 101.6296 14.74754903101120
| Epoch (UTC): | 05 October 2024 20:22:07 |
| Eccentricity: | 0.0118526 |
| inclination: | 98.5180° |
| perigee height: | 562 km |
| apogee height: | 729 km |
| right ascension of ascending node: | 317.8966° |
| argument of perigee: | 257.1647° |
| revolutions per day: | 14.74754903 |
| mean anomaly at epoch: | 101.6296° |
| orbit number at epoch: | 10112 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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