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 22618U 93016AC 22176.80256754 .00000161 00000-0 17309-3 0 9994
2 22618 70.9933 314.4998 0159020 232.6687 125.9842 13.82240828473699
| Epoch (UTC): | 25 June 2022 19:15:41 |
| Eccentricity: | 0.0159020 |
| inclination: | 70.9933° |
| perigee height: | 839 km |
| apogee height: | 1072 km |
| right ascension of ascending node: | 314.4998° |
| argument of perigee: | 232.6687° |
| revolutions per day: | 13.82240828 |
| mean anomaly at epoch: | 125.9842° |
| orbit number at epoch: | 47369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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