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 50806U 26145.45382626 +.00000000 +00000-0 -64671-4 0 00005
2 50806 53.2113 174.5135 0001236 78.9979 281.1152 15.08825616 05
| Epoch (UTC): | 25 May 2026 10:53:30 |
| Eccentricity: | 0.0001236 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 174.5135° |
| argument of perigee: | 78.9979° |
| revolutions per day: | 15.08825616 |
| mean anomaly at epoch: | 281.1152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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