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 22207U 26053.73454219 +.00000000 +00000-0 +45045-4 0 00009
2 22207 82.9192 220.2904 0031687 320.7733 65.6786 13.73082162 06
| Epoch (UTC): | 22 February 2026 17:37:44 |
| Eccentricity: | 0.0031687 |
| inclination: | 82.9192° |
| perigee height: | 965 km |
| apogee height: | 1012 km |
| right ascension of ascending node: | 220.2904° |
| argument of perigee: | 320.7733° |
| revolutions per day: | 13.73082162 |
| mean anomaly at epoch: | 65.6786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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