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 26048.79157980 +.00000000 +00000-0 +49932-4 0 00005
2 00050 47.2292 172.3243 0113005 19.1604 341.3388 12.20162816 05
| Epoch (UTC): | 17 February 2026 18:59:52 |
| Eccentricity: | 0.0113005 |
| inclination: | 47.2292° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 172.3243° |
| argument of perigee: | 19.1604° |
| revolutions per day: | 12.20162816 |
| mean anomaly at epoch: | 341.3388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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