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 48564U 26145.42627446 +.00000000 +00000-0 +58038-4 0 00001
2 48564 53.1579 129.8012 0001226 84.4659 275.6483 15.31708014 04
| Epoch (UTC): | 25 May 2026 10:13:50 |
| Eccentricity: | 0.0001226 |
| inclination: | 53.1579° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 129.8012° |
| argument of perigee: | 84.4659° |
| revolutions per day: | 15.31708014 |
| mean anomaly at epoch: | 275.6483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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