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 48575U 26145.24464060 +.00000000 +00000-0 -10221-4 0 00007
2 48575 53.1605 92.1570 0001559 94.4952 265.6227 15.31697971 07
| Epoch (UTC): | 25 May 2026 05:52:16 |
| Eccentricity: | 0.0001559 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 92.1570° |
| argument of perigee: | 94.4952° |
| revolutions per day: | 15.31697971 |
| mean anomaly at epoch: | 265.6227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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