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 50483U 26145.43126731 +.00000000 +00000-0 +15159-3 0 00002
2 50483 87.9170 339.9835 0001944 90.8119 269.3236 13.18687275 09
| Epoch (UTC): | 25 May 2026 10:21:01 |
| Eccentricity: | 0.0001944 |
| inclination: | 87.9170° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9835° |
| argument of perigee: | 90.8119° |
| revolutions per day: | 13.18687275 |
| mean anomaly at epoch: | 269.3236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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