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 52346U 26145.41428463 +.00000000 +00000-0 -57922-4 0 00003
2 52346 53.2125 214.6979 0001272 92.0708 268.0429 15.08834746 03
| Epoch (UTC): | 25 May 2026 09:56:34 |
| Eccentricity: | 0.0001272 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 214.6979° |
| argument of perigee: | 92.0708° |
| revolutions per day: | 15.08834746 |
| mean anomaly at epoch: | 268.0429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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