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 26066.79122814 +.00000000 +00000-0 +96671-4 0 00004
2 22208 82.9225 174.0328 0035154 151.0011 323.6941 13.75431997 03
| Epoch (UTC): | 07 March 2026 18:59:22 |
| Eccentricity: | 0.0035154 |
| inclination: | 82.9225° |
| perigee height: | 954 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 174.0328° |
| argument of perigee: | 151.0011° |
| revolutions per day: | 13.75431997 |
| mean anomaly at epoch: | 323.6941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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