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 48411U 26144.83828282 +.00000000 +00000-0 +28818-3 0 00009
2 48411 53.1593 299.6879 0001123 80.8891 279.2237 15.31713976 02
| Epoch (UTC): | 24 May 2026 20:07:07 |
| Eccentricity: | 0.0001123 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 299.6879° |
| argument of perigee: | 80.8891° |
| revolutions per day: | 15.31713976 |
| mean anomaly at epoch: | 279.2237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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