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 data is extracted from the following two-line orbital elements,
1 11416U 79057A 23159.49392743 .00000415 00000-0 16448-3 0 9998
2 11416 98.6511 175.7780 0009092 290.3213 69.6994 14.34063161292544
| Epoch (UTC): | 08 June 2023 11:51:15 |
| Eccentricity: | 0.0009092 |
| inclination: | 98.6511° |
| perigee height: | 771 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 175.7780° |
| argument of perigee: | 290.3213° |
| revolutions per day: | 14.34063161 |
| mean anomaly at epoch: | 69.6994° |
| orbit number at epoch: | 29254 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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