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 52569U 26145.27349145 +.00000000 +00000-0 +13122-4 0 00006
2 52569 53.2128 135.3237 0001160 82.8346 277.2778 15.08833941 05
| Epoch (UTC): | 25 May 2026 06:33:49 |
| Eccentricity: | 0.0001160 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 135.3237° |
| argument of perigee: | 82.8346° |
| revolutions per day: | 15.08833941 |
| mean anomaly at epoch: | 277.2778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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