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 26127.85704191 +.00000000 +00000-0 +97990-4 0 00001
2 27422 98.5928 65.7814 0012268 18.9750 341.1888 14.31062612 09
| Epoch (UTC): | 07 May 2026 20:34:08 |
| Eccentricity: | 0.0012268 |
| inclination: | 98.5928° |
| perigee height: | 779 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 65.7814° |
| argument of perigee: | 18.9750° |
| revolutions per day: | 14.31062612 |
| mean anomaly at epoch: | 341.1888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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