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 22220U 26044.69476998 +.00000000 +00000-0 -58378-4 0 00001
2 22220 70.9977 238.9184 0011274 139.7018 292.3498 14.16855674 02
| Epoch (UTC): | 13 February 2026 16:40:28 |
| Eccentricity: | 0.0011274 |
| inclination: | 70.9977° |
| perigee height: | 828 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 238.9184° |
| argument of perigee: | 139.7018° |
| revolutions per day: | 14.16855674 |
| mean anomaly at epoch: | 292.3498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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