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 22049U 26152.34256179 +.00000000 +00000-0 +00000-0 0 00003
2 22049 45.3301 344.9691 5749824 280.4219 357.9274 0.19173402 00
| Epoch (UTC): | 01 June 2026 08:13:17 |
| Eccentricity: | 0.5749824 |
| inclination: | 45.3301° |
| perigee height: | 47616 km |
| apogee height: | 193706 km |
| right ascension of ascending node: | 344.9691° |
| argument of perigee: | 280.4219° |
| revolutions per day: | 0.19173402 |
| mean anomaly at epoch: | 357.9274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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