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 41168U 15077C 23220.21009196 .06493376 -26828-4 29602-2 0 9997
2 41168 14.9794 162.8281 0006365 225.0533 134.9286 16.20615855424534
| Epoch (UTC): | 08 August 2023 05:02:31 |
| Eccentricity: | 0.0006365 |
| inclination: | 14.9794° |
| perigee height: | 213 km |
| apogee height: | 222 km |
| right ascension of ascending node: | 162.8281° |
| argument of perigee: | 225.0533° |
| revolutions per day: | 16.20615855 |
| mean anomaly at epoch: | 134.9286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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