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 52132U 26145.52096868 +.00000000 +00000-0 -19181-4 0 00003
2 52132 53.2130 84.2089 0001223 64.8252 295.2867 15.08836064 05
| Epoch (UTC): | 25 May 2026 12:30:11 |
| Eccentricity: | 0.0001223 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 84.2089° |
| argument of perigee: | 64.8252° |
| revolutions per day: | 15.08836064 |
| mean anomaly at epoch: | 295.2867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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