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 26134.78689400 +.00000000 +00000-0 -29074-3 0 00002
2 00050 47.2317 265.3998 0113540 275.1615 83.6226 12.20164623 08
| Epoch (UTC): | 14 May 2026 18:53:07 |
| Eccentricity: | 0.0113540 |
| inclination: | 47.2317° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 265.3998° |
| argument of perigee: | 275.1615° |
| revolutions per day: | 12.20164623 |
| mean anomaly at epoch: | 83.6226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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