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 52576U 26145.38484166 +.00000000 +00000-0 +52521-4 0 00005
2 52576 53.2130 134.8201 0001094 70.4746 289.6364 15.08835520 07
| Epoch (UTC): | 25 May 2026 09:14:10 |
| Eccentricity: | 0.0001094 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 134.8201° |
| argument of perigee: | 70.4746° |
| revolutions per day: | 15.08835520 |
| mean anomaly at epoch: | 289.6364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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