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 22018.59574554 -.00000056 00000-0 26990-3 0 9998
2 00050 47.2312 120.6979 0113981 254.4571 104.3610 12.20118177741053
| Epoch (UTC): | 18 January 2022 14:17:52 |
| Eccentricity: | 0.0113981 |
| inclination: | 47.2312° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 120.6979° |
| argument of perigee: | 254.4571° |
| revolutions per day: | 12.20118177 |
| mean anomaly at epoch: | 104.3610° |
| orbit number at epoch: | 74105 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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