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 40379U 15003D 24052.92188328 .09430395 37124-5 76406-3 0 9997
2 40379 99.0545 64.0391 0006905 151.9068 208.2600 16.39942224502311
| Epoch (UTC): | 21 February 2024 22:07:30 |
| Eccentricity: | 0.0006905 |
| inclination: | 99.0545° |
| perigee height: | 161 km |
| apogee height: | 170 km |
| right ascension of ascending node: | 64.0391° |
| argument of perigee: | 151.9068° |
| revolutions per day: | 16.39942224 |
| mean anomaly at epoch: | 208.2600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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