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 50845U 26145.34892661 +.00000000 +00000-0 +31752-3 0 00003
2 50845 53.2112 194.9841 0000962 79.0067 281.1033 15.08814450 04
| Epoch (UTC): | 25 May 2026 08:22:27 |
| Eccentricity: | 0.0000962 |
| inclination: | 53.2112° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 194.9841° |
| argument of perigee: | 79.0067° |
| revolutions per day: | 15.08814450 |
| mean anomaly at epoch: | 281.1033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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