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 48566U 26145.29211279 +.00000000 +00000-0 +61014-4 0 00009
2 48566 53.1603 152.6242 0001192 85.8795 274.2343 15.31706191 05
| Epoch (UTC): | 25 May 2026 07:00:38 |
| Eccentricity: | 0.0001192 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 152.6242° |
| argument of perigee: | 85.8795° |
| revolutions per day: | 15.31706191 |
| mean anomaly at epoch: | 274.2343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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