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 26131.67467139 +.00000000 +00000-0 +19456-4 0 00003
2 00050 47.2318 275.0595 0113523 265.9277 92.8530 12.20164683 08
| Epoch (UTC): | 11 May 2026 16:11:31 |
| Eccentricity: | 0.0113523 |
| inclination: | 47.2318° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 275.0595° |
| argument of perigee: | 265.9277° |
| revolutions per day: | 12.20164683 |
| mean anomaly at epoch: | 92.8530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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