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 is defined by the following mean orbital elements,
1 48543U 10057BN 24272.29199459 .00002630 00000-0 62661-2 0 9996
2 48543 21.4669 326.7114 7036307 279.4978 13.5684 2.50539765 92167
| Epoch (UTC): | 28 September 2024 07:00:28 |
| Eccentricity: | 0.7036307 |
| inclination: | 21.4669° |
| perigee height: | 408 km |
| apogee height: | 32633 km |
| right ascension of ascending node: | 326.7114° |
| argument of perigee: | 279.4978° |
| revolutions per day: | 2.50539765 |
| mean anomaly at epoch: | 13.5684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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