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 22078U 26104.21455331 +.00000000 +00000-0 -19602-4 0 00002
2 22078 66.0870 42.5245 0015721 297.2024 62.7392 12.86851688 04
| Epoch (UTC): | 14 April 2026 05:08:57 |
| Eccentricity: | 0.0015721 |
| inclination: | 66.0870° |
| perigee height: | 1302 km |
| apogee height: | 1326 km |
| right ascension of ascending node: | 42.5245° |
| argument of perigee: | 297.2024° |
| revolutions per day: | 12.86851688 |
| mean anomaly at epoch: | 62.7392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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