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 50497U 26145.28795034 +.00000000 +00000-0 -34147-2 0 00006
2 50497 87.9167 340.0115 0001462 108.5257 251.6034 13.18694248 07
| Epoch (UTC): | 25 May 2026 06:54:38 |
| Eccentricity: | 0.0001462 |
| inclination: | 87.9167° |
| perigee height: | 1189 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0115° |
| argument of perigee: | 108.5257° |
| revolutions per day: | 13.18694248 |
| mean anomaly at epoch: | 251.6034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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