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 26022.49120194 +.00000000 +00000-0 +64463-3 0 00005
2 00022 50.2395 98.8021 0085034 258.5185 100.6216 15.24946204 05
| Epoch (UTC): | 22 January 2026 11:47:19 |
| Eccentricity: | 0.0085034 |
| inclination: | 50.2395° |
| perigee height: | 433 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 98.8021° |
| argument of perigee: | 258.5185° |
| revolutions per day: | 15.24946204 |
| mean anomaly at epoch: | 100.6216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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