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 48546U 11077AS 24320.24161708 .00000073 00000-0 20970-1 0 9992
2 48546 20.1388 185.0298 7366554 218.5572 54.2335 1.85903440 30874
| Epoch (UTC): | 15 November 2024 05:47:55 |
| Eccentricity: | 0.7366554 |
| inclination: | 20.1388° |
| perigee height: | 979 km |
| apogee height: | 42142 km |
| right ascension of ascending node: | 185.0298° |
| argument of perigee: | 218.5572° |
| revolutions per day: | 1.85903440 |
| mean anomaly at epoch: | 54.2335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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