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 26041.09660389 +.00000000 +00000-0 +65604-3 0 00005
2 00022 50.2472 7.2837 0083605 333.1560 26.5085 15.25710750 05
| Epoch (UTC): | 10 February 2026 02:19:06 |
| Eccentricity: | 0.0083605 |
| inclination: | 50.2472° |
| perigee height: | 431 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 7.2837° |
| argument of perigee: | 333.1560° |
| revolutions per day: | 15.25710750 |
| mean anomaly at epoch: | 26.5085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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