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 40378U 15003C 23213.46747684 .09535059 37184-5 78516-3 0 9992
2 40378 99.0570 187.9460 0006954 206.7965 153.2971 16.39803081471850
| Epoch (UTC): | 01 August 2023 11:13:09 |
| Eccentricity: | 0.0006954 |
| inclination: | 99.0570° |
| perigee height: | 162 km |
| apogee height: | 171 km |
| right ascension of ascending node: | 187.9460° |
| argument of perigee: | 206.7965° |
| revolutions per day: | 16.39803081 |
| mean anomaly at epoch: | 153.2971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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