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 50190U 26145.27717266 +.00000000 +00000-0 -21402-4 0 00008
2 50190 53.2146 255.3052 0001333 90.7624 269.3521 15.08835571 09
| Epoch (UTC): | 25 May 2026 06:39:07 |
| Eccentricity: | 0.0001333 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 255.3052° |
| argument of perigee: | 90.7624° |
| revolutions per day: | 15.08835571 |
| mean anomaly at epoch: | 269.3521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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