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 00050U 60009B 23087.76626925 -.00000095 00000-0 -85727-4 0 9992
2 00050 47.2298 213.1598 0113673 108.9752 252.3394 12.20128057794063
| Epoch (UTC): | 28 March 2023 18:23:25 |
| Eccentricity: | 0.0113673 |
| inclination: | 47.2298° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 213.1598° |
| argument of perigee: | 108.9752° |
| revolutions per day: | 12.20128057 |
| mean anomaly at epoch: | 252.3394° |
| orbit number at epoch: | 79406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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