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 52557U 26145.29098516 +.00000000 +00000-0 -29329-3 0 00004
2 52557 53.2122 145.2466 0001045 86.5133 273.5979 15.08836798 02
| Epoch (UTC): | 25 May 2026 06:59:01 |
| Eccentricity: | 0.0001045 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 145.2466° |
| argument of perigee: | 86.5133° |
| revolutions per day: | 15.08836798 |
| mean anomaly at epoch: | 273.5979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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