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 00022U 26104.32235389 +.00000000 +00000-0 +20128-3 0 00001
2 00022 50.2446 55.6182 0079736 227.0893 132.3357 15.27635970 06
| Epoch (UTC): | 14 April 2026 07:44:11 |
| Eccentricity: | 0.0079736 |
| inclination: | 50.2446° |
| perigee height: | 428 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 55.6182° |
| argument of perigee: | 227.0893° |
| revolutions per day: | 15.27635970 |
| mean anomaly at epoch: | 132.3357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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