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 50197U 26145.33235191 +.00000000 +00000-0 +13566-3 0 00004
2 50197 53.2150 255.0580 0001007 88.0303 272.0804 15.08851554 00
| Epoch (UTC): | 25 May 2026 07:58:35 |
| Eccentricity: | 0.0001007 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 255.0580° |
| argument of perigee: | 88.0303° |
| revolutions per day: | 15.08851554 |
| mean anomaly at epoch: | 272.0804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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