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 52684U 26145.32454516 +.00000000 +00000-0 +13315-4 0 00003
2 52684 53.2130 160.0940 0001264 77.1243 282.9890 15.08840018 01
| Epoch (UTC): | 25 May 2026 07:47:20 |
| Eccentricity: | 0.0001264 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 160.0940° |
| argument of perigee: | 77.1243° |
| revolutions per day: | 15.08840018 |
| mean anomaly at epoch: | 282.9890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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