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 22221.71703548 -.00000061 00000-0 23095-3 0 9994
2 00050 47.2283 210.2720 0112994 140.3433 220.5685 12.20121583765855
| Epoch (UTC): | 09 August 2022 17:12:31 |
| Eccentricity: | 0.0112994 |
| inclination: | 47.2283° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 210.2720° |
| argument of perigee: | 140.3433° |
| revolutions per day: | 12.20121583 |
| mean anomaly at epoch: | 220.5685° |
| orbit number at epoch: | 76585 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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