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 22208U 26072.76744310 +.00000000 +00000-0 +59403-4 0 00001
2 22208 82.9224 169.5905 0035456 134.7549 34.8330 13.75432925 06
| Epoch (UTC): | 13 March 2026 18:25:07 |
| Eccentricity: | 0.0035456 |
| inclination: | 82.9224° |
| perigee height: | 954 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 169.5905° |
| argument of perigee: | 134.7549° |
| revolutions per day: | 13.75432925 |
| mean anomaly at epoch: | 34.8330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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