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 50809U 26145.45012860 +.00000000 +00000-0 -17790-3 0 00007
2 50809 53.2115 174.5317 0001150 102.9372 257.1748 15.08849538 05
| Epoch (UTC): | 25 May 2026 10:48:11 |
| Eccentricity: | 0.0001150 |
| inclination: | 53.2115° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 174.5317° |
| argument of perigee: | 102.9372° |
| revolutions per day: | 15.08849538 |
| mean anomaly at epoch: | 257.1748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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