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 52341U 26145.39768670 +.00000000 +00000-0 +15376-3 0 00007
2 52341 53.2136 224.7166 0001112 81.6102 278.5016 15.08846523 09
| Epoch (UTC): | 25 May 2026 09:32:40 |
| Eccentricity: | 0.0001112 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 224.7166° |
| argument of perigee: | 81.6102° |
| revolutions per day: | 15.08846523 |
| mean anomaly at epoch: | 278.5016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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