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 50474U 26145.25928418 +.00000000 +00000-0 +10728-3 0 00001
2 50474 87.9168 340.0044 0002071 89.5097 270.6273 13.18688323 04
| Epoch (UTC): | 25 May 2026 06:13:22 |
| Eccentricity: | 0.0002071 |
| inclination: | 87.9168° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0044° |
| argument of perigee: | 89.5097° |
| revolutions per day: | 13.18688323 |
| mean anomaly at epoch: | 270.6273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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