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 22915U 26146.23414947 +.00000000 +00000-0 +00000-0 0 00005
2 22915 13.7724 15.6274 0006879 13.8787 342.8900 0.98533852 03
| Epoch (UTC): | 26 May 2026 05:37:10 |
| Eccentricity: | 0.0006879 |
| inclination: | 13.7724° |
| perigee height: | 36252 km |
| apogee height: | 36310 km |
| right ascension of ascending node: | 15.6274° |
| argument of perigee: | 13.8787° |
| revolutions per day: | 0.98533852 |
| mean anomaly at epoch: | 342.8900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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