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 26044.58981647 +.00000000 +00000-0 +49352-4 0 00001
2 18422 82.5084 89.8753 0020311 90.7433 269.6111 14.85305609 06
| Epoch (UTC): | 13 February 2026 14:09:20 |
| Eccentricity: | 0.0020311 |
| inclination: | 82.5084° |
| perigee height: | 598 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 89.8753° |
| argument of perigee: | 90.7433° |
| revolutions per day: | 14.85305609 |
| mean anomaly at epoch: | 269.6111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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