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 50321U 26144.45884933 +.00000000 +00000-0 +00000-0 0 00005
2 50321 3.6157 80.2207 0003851 284.4923 122.5746 1.00037720 00
| Epoch (UTC): | 24 May 2026 11:00:44 |
| Eccentricity: | 0.0003851 |
| inclination: | 3.6157° |
| perigee height: | 35836 km |
| apogee height: | 35869 km |
| right ascension of ascending node: | 80.2207° |
| argument of perigee: | 284.4923° |
| revolutions per day: | 1.00037720 |
| mean anomaly at epoch: | 122.5746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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