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 52843U 26145.02922792 +.00000000 +00000-0 -15875-4 0 00007
2 52843 53.2141 51.4196 0001484 78.1793 281.9365 15.08840106 05
| Epoch (UTC): | 25 May 2026 00:42:05 |
| Eccentricity: | 0.0001484 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 51.4196° |
| argument of perigee: | 78.1793° |
| revolutions per day: | 15.08840106 |
| mean anomaly at epoch: | 281.9365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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