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 22519U 92086C 25273.82161507 0.00011500 00000-0 16436-2 0 05
2 22519 56.9005 149.7809 3016586 65.1173 294.8827 9.17228680 09
| Epoch (UTC): | 30 September 2025 19:43:07 |
| Eccentricity: | 0.3016586 |
| inclination: | 56.9005° |
| perigee height: | 354 km |
| apogee height: | 6170 km |
| right ascension of ascending node: | 149.7809° |
| argument of perigee: | 65.1173° |
| revolutions per day: | 9.17228680 |
| mean anomaly at epoch: | 294.8827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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