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 48274U 26108.62114575 +.00000000 +00000-0 +27268-3 0 00004
2 48274 41.4677 324.8359 0006259 233.0433 126.9834 15.62526922 03
| Epoch (UTC): | 18 April 2026 14:54:26 |
| Eccentricity: | 0.0006259 |
| inclination: | 41.4677° |
| perigee height: | 376 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 324.8359° |
| argument of perigee: | 233.0433° |
| revolutions per day: | 15.62526922 |
| mean anomaly at epoch: | 126.9834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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