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 00050U 26046.82593457 +.00000000 +00000-0 +26088-3 0 00006
2 00050 47.2291 178.4256 0113048 13.3075 347.0657 12.20162784 06
| Epoch (UTC): | 15 February 2026 19:49:20 |
| Eccentricity: | 0.0113048 |
| inclination: | 47.2291° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 178.4256° |
| argument of perigee: | 13.3075° |
| revolutions per day: | 12.20162784 |
| mean anomaly at epoch: | 347.0657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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