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 43855U 18104G 24134.35325181 .12320967 -15037-5 27872-3 0 9992
2 43855 84.9866 294.2530 0011178 259.2513 100.7537 16.45723631302149
| Epoch (UTC): | 13 May 2024 08:28:40 |
| Eccentricity: | 0.0011178 |
| inclination: | 84.9866° |
| perigee height: | 143 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 294.2530° |
| argument of perigee: | 259.2513° |
| revolutions per day: | 16.45723631 |
| mean anomaly at epoch: | 100.7537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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