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 40377U 15003B 23212.82834728 .10819241 37387-5 80657-3 0 9990
2 40377 99.0456 186.7613 0007269 195.9689 164.1377 16.40629520471746
| Epoch (UTC): | 31 July 2023 19:52:49 |
| Eccentricity: | 0.0007269 |
| inclination: | 99.0456° |
| perigee height: | 159 km |
| apogee height: | 169 km |
| right ascension of ascending node: | 186.7613° |
| argument of perigee: | 195.9689° |
| revolutions per day: | 16.40629520 |
| mean anomaly at epoch: | 164.1377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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