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 26140.60185772 +.00000000 +00000-0 +69211-3 0 00009
2 00050 47.2313 247.3508 0113549 292.4325 66.4471 12.20164831 02
| Epoch (UTC): | 20 May 2026 14:26:40 |
| Eccentricity: | 0.0113549 |
| inclination: | 47.2313° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 247.3508° |
| argument of perigee: | 292.4325° |
| revolutions per day: | 12.20164831 |
| mean anomaly at epoch: | 66.4471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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