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 50490U 26145.27108660 +.00000000 +00000-0 +73306-4 0 00002
2 50490 87.9159 340.0180 0001804 79.4630 280.6705 13.18687151 06
| Epoch (UTC): | 25 May 2026 06:30:21 |
| Eccentricity: | 0.0001804 |
| inclination: | 87.9159° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0180° |
| argument of perigee: | 79.4630° |
| revolutions per day: | 13.18687151 |
| mean anomaly at epoch: | 280.6705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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