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 50808U 26145.38020902 +.00000000 +00000-0 -13948-3 0 00005
2 50808 53.2102 174.8440 0001189 82.7522 277.3605 15.08848071 01
| Epoch (UTC): | 25 May 2026 09:07:30 |
| Eccentricity: | 0.0001189 |
| inclination: | 53.2102° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 174.8440° |
| argument of perigee: | 82.7522° |
| revolutions per day: | 15.08848071 |
| mean anomaly at epoch: | 277.3605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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