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 22719U 26146.13716352 +.00000000 +00000-0 +00000-0 0 00001
2 22719 13.8891 14.3412 0001963 32.7061 160.8899 0.99048568 06
| Epoch (UTC): | 26 May 2026 03:17:30 |
| Eccentricity: | 0.0001963 |
| inclination: | 13.8891° |
| perigee height: | 36125 km |
| apogee height: | 36141 km |
| right ascension of ascending node: | 14.3412° |
| argument of perigee: | 32.7061° |
| revolutions per day: | 0.99048568 |
| mean anomaly at epoch: | 160.8899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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