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 26044.30578426 +.00000000 +00000-0 +63484-3 0 00006
2 00022 50.2476 351.4889 0083319 346.0790 13.7873 15.25832942 01
| Epoch (UTC): | 13 February 2026 07:20:19 |
| Eccentricity: | 0.0083319 |
| inclination: | 50.2476° |
| perigee height: | 431 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 351.4889° |
| argument of perigee: | 346.0790° |
| revolutions per day: | 15.25832942 |
| mean anomaly at epoch: | 13.7873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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