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 52347U 26145.49156659 +.00000000 +00000-0 -13541-3 0 00005
2 52347 53.2130 214.3528 0001168 97.6507 262.4618 15.08848100 06
| Epoch (UTC): | 25 May 2026 11:47:51 |
| Eccentricity: | 0.0001168 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 214.3528° |
| argument of perigee: | 97.6507° |
| revolutions per day: | 15.08848100 |
| mean anomaly at epoch: | 262.4618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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