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 52446U 26145.62247697 +.00000000 +00000-0 +76420-3 0 00007
2 52446 97.5687 257.9626 0002375 137.4612 222.6834 15.70313518 04
| Epoch (UTC): | 25 May 2026 14:56:22 |
| Eccentricity: | 0.0002375 |
| inclination: | 97.5687° |
| perigee height: | 356 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 257.9626° |
| argument of perigee: | 137.4612° |
| revolutions per day: | 15.70313518 |
| mean anomaly at epoch: | 222.6834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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