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 27422U 26106.67179124 +.00000000 +00000-0 +67305-4 0 00007
2 27422 98.5912 44.8345 0012993 76.6548 283.6083 14.31051257 00
| Epoch (UTC): | 16 April 2026 16:07:22 |
| Eccentricity: | 0.0012993 |
| inclination: | 98.5912° |
| perigee height: | 779 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 44.8345° |
| argument of perigee: | 76.6548° |
| revolutions per day: | 14.31051257 |
| mean anomaly at epoch: | 283.6083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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