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 50192U 26144.80980733 +.00000000 +00000-0 +25853-4 0 00002
2 50192 53.2144 257.3995 0001256 110.6897 249.4230 15.08836401 04
| Epoch (UTC): | 24 May 2026 19:26:07 |
| Eccentricity: | 0.0001256 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 257.3995° |
| argument of perigee: | 110.6897° |
| revolutions per day: | 15.08836401 |
| mean anomaly at epoch: | 249.4230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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