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 26075.74965147 +.00000000 +00000-0 +44974-4 0 00002
2 22208 82.9221 167.3738 0035587 126.6560 41.1895 13.75433140 08
| Epoch (UTC): | 16 March 2026 17:59:29 |
| Eccentricity: | 0.0035587 |
| inclination: | 82.9221° |
| perigee height: | 954 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 167.3738° |
| argument of perigee: | 126.6560° |
| revolutions per day: | 13.75433140 |
| mean anomaly at epoch: | 41.1895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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