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 49950U 26145.41530727 +.00000000 +00000-0 +38346-3 0 00004
2 49950 41.9942 188.1781 0009806 83.4508 276.7451 15.49026722 03
| Epoch (UTC): | 25 May 2026 09:58:02 |
| Eccentricity: | 0.0009806 |
| inclination: | 41.9942° |
| perigee height: | 413 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 188.1781° |
| argument of perigee: | 83.4508° |
| revolutions per day: | 15.49026722 |
| mean anomaly at epoch: | 276.7451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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