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 26074.72818508 +.00000000 +00000-0 +39496-4 0 00000
2 22208 82.9222 168.1330 0035532 129.4244 23.4203 13.75433018 06
| Epoch (UTC): | 15 March 2026 17:28:35 |
| Eccentricity: | 0.0035532 |
| inclination: | 82.9222° |
| perigee height: | 954 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 168.1330° |
| argument of perigee: | 129.4244° |
| revolutions per day: | 13.75433018 |
| mean anomaly at epoch: | 23.4203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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