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 52535U 26145.15112891 +.00000000 +00000-0 +22643-4 0 00000
2 52535 53.2139 145.8694 0001002 66.1894 293.9203 15.08846769 01
| Epoch (UTC): | 25 May 2026 03:37:37 |
| Eccentricity: | 0.0001002 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 145.8694° |
| argument of perigee: | 66.1894° |
| revolutions per day: | 15.08846769 |
| mean anomaly at epoch: | 293.9203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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