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 22331.80966058 .00000142 00000-0 15624-3 0 9999
2 22618 70.9936 6.0086 0157604 8.2443 352.1195 13.82313142495113
| Epoch (UTC): | 27 November 2022 19:25:54 |
| Eccentricity: | 0.0157604 |
| inclination: | 70.9936° |
| perigee height: | 840 km |
| apogee height: | 1071 km |
| right ascension of ascending node: | 6.0086° |
| argument of perigee: | 8.2443° |
| revolutions per day: | 13.82313142 |
| mean anomaly at epoch: | 352.1195° |
| orbit number at epoch: | 49511 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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