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 50500U 26145.50039096 +.00000000 +00000-0 +11653-3 0 00002
2 50500 87.9162 339.9751 0001718 85.6520 274.4808 13.18688974 03
| Epoch (UTC): | 25 May 2026 12:00:33 |
| Eccentricity: | 0.0001718 |
| inclination: | 87.9162° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9751° |
| argument of perigee: | 85.6520° |
| revolutions per day: | 13.18688974 |
| mean anomaly at epoch: | 274.4808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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