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 36869U 10039B 22222.51959874 .00005925 00000-0 75360-3 0 9998
2 36869 20.1537 323.4726 4767458 357.4925 0.7752 6.02951084199493
| Epoch (UTC): | 10 August 2022 12:28:13 |
| Eccentricity: | 0.4767458 |
| inclination: | 20.1537° |
| perigee height: | 294 km |
| apogee height: | 12452 km |
| right ascension of ascending node: | 323.4726° |
| argument of perigee: | 357.4925° |
| revolutions per day: | 6.02951084 |
| mean anomaly at epoch: | 0.7752° |
| orbit number at epoch: | 19949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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