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 52690U 26145.30614503 +.00000000 +00000-0 +74188-4 0 00007
2 52690 53.2133 160.1743 0001020 76.7547 283.3559 15.08841492 09
| Epoch (UTC): | 25 May 2026 07:20:50 |
| Eccentricity: | 0.0001020 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 160.1743° |
| argument of perigee: | 76.7547° |
| revolutions per day: | 15.08841492 |
| mean anomaly at epoch: | 283.3559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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