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 50812U 26145.47589812 +.00000000 +00000-0 +64690-4 0 00000
2 50812 53.2130 174.5191 0001087 47.9477 312.1607 15.08840436 03
| Epoch (UTC): | 25 May 2026 11:25:17 |
| Eccentricity: | 0.0001087 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 174.5191° |
| argument of perigee: | 47.9477° |
| revolutions per day: | 15.08840436 |
| mean anomaly at epoch: | 312.1607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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