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 50472U 26145.60349656 +.00000000 +00000-0 -72117-4 0 00001
2 50472 87.9162 10.3366 0002160 90.8347 269.3032 13.17648909 05
| Epoch (UTC): | 25 May 2026 14:29:02 |
| Eccentricity: | 0.0002160 |
| inclination: | 87.9162° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3366° |
| argument of perigee: | 90.8347° |
| revolutions per day: | 13.17648909 |
| mean anomaly at epoch: | 269.3032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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