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 50481U 26145.29132251 +.00000000 +00000-0 -92936-4 0 00008
2 50481 87.9171 339.9976 0001860 80.9635 279.1708 13.18687633 05
| Epoch (UTC): | 25 May 2026 06:59:30 |
| Eccentricity: | 0.0001860 |
| inclination: | 87.9171° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9976° |
| argument of perigee: | 80.9635° |
| revolutions per day: | 13.18687633 |
| mean anomaly at epoch: | 279.1708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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