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 14506U 83113A 23151.48444435 .00000293 00000-0 13329-3 0 9995
2 14506 98.2978 326.8629 0009836 279.6642 138.7217 14.28514862 56550
| Epoch (UTC): | 31 May 2023 11:37:35 |
| Eccentricity: | 0.0009836 |
| inclination: | 98.2978° |
| perigee height: | 789 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 326.8629° |
| argument of perigee: | 279.6642° |
| revolutions per day: | 14.28514862 |
| mean anomaly at epoch: | 138.7217° |
| orbit number at epoch: | 5655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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