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 50476U 26145.48016782 +.00000000 +00000-0 +11920-3 0 00005
2 50476 87.9170 339.9732 0002014 88.4774 271.6589 13.18687925 05
| Epoch (UTC): | 25 May 2026 11:31:26 |
| Eccentricity: | 0.0002014 |
| inclination: | 87.9170° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9732° |
| argument of perigee: | 88.4774° |
| revolutions per day: | 13.18687925 |
| mean anomaly at epoch: | 271.6589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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