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 is defined by the following mean orbital elements,
1 18422U 26161.60336509 +.00000000 +00000-0 +41129-4 0 00009
2 18422 82.5105 339.7858 0020068 65.7376 294.5933 14.85408177 03
| Epoch (UTC): | 10 June 2026 14:28:50 |
| Eccentricity: | 0.0020068 |
| inclination: | 82.5105° |
| perigee height: | 598 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 339.7858° |
| argument of perigee: | 65.7376° |
| revolutions per day: | 14.85408177 |
| mean anomaly at epoch: | 294.5933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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