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 50822U 26145.38296613 +.00000000 +00000-0 +36921-4 0 00001
2 50822 53.2115 184.8312 0001156 74.7338 285.3782 15.08839367 03
| Epoch (UTC): | 25 May 2026 09:11:28 |
| Eccentricity: | 0.0001156 |
| inclination: | 53.2115° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 184.8312° |
| argument of perigee: | 74.7338° |
| revolutions per day: | 15.08839367 |
| mean anomaly at epoch: | 285.3782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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