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 22219.42376402 -.00000085 00000-0 11556-4 0 9990
2 00050 47.2281 217.3901 0112993 133.5046 227.5200 12.20121479765578
| Epoch (UTC): | 07 August 2022 10:10:13 |
| Eccentricity: | 0.0112993 |
| inclination: | 47.2281° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 217.3901° |
| argument of perigee: | 133.5046° |
| revolutions per day: | 12.20121479 |
| mean anomaly at epoch: | 227.5200° |
| orbit number at epoch: | 76557 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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