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 26154.42578323 +.00000000 +00000-0 +11809-3 0 00004
2 27422 98.5941 92.0582 0010753 298.8139 61.1964 14.31075278 02
| Epoch (UTC): | 03 June 2026 10:13:07 |
| Eccentricity: | 0.0010753 |
| inclination: | 98.5941° |
| perigee height: | 780 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 92.0582° |
| argument of perigee: | 298.8139° |
| revolutions per day: | 14.31075278 |
| mean anomaly at epoch: | 61.1964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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