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 00829U 64038A 22228.70624316 .00000581 00000-0 17755-3 0 9997
2 00829 60.8238 331.0769 2970014 335.6891 12.8057 9.14757384886839
| Epoch (UTC): | 16 August 2022 16:56:59 |
| Eccentricity: | 0.2970014 |
| inclination: | 60.8238° |
| perigee height: | 411 km |
| apogee height: | 6147 km |
| right ascension of ascending node: | 331.0769° |
| argument of perigee: | 335.6891° |
| revolutions per day: | 9.14757384 |
| mean anomaly at epoch: | 12.8057° |
| orbit number at epoch: | 88683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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