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 52562U 26145.41332928 +.00000000 +00000-0 +23854-4 0 00009
2 52562 53.2137 134.6933 0001191 71.9150 288.1972 15.08838838 06
| Epoch (UTC): | 25 May 2026 09:55:11 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 134.6933° |
| argument of perigee: | 71.9150° |
| revolutions per day: | 15.08838838 |
| mean anomaly at epoch: | 288.1972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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