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 50503U 26145.28120507 +.00000000 +00000-0 +47203-4 0 00009
2 50503 87.9170 340.0114 0001892 78.3496 281.7849 13.18687888 04
| Epoch (UTC): | 25 May 2026 06:44:56 |
| Eccentricity: | 0.0001892 |
| inclination: | 87.9170° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0114° |
| argument of perigee: | 78.3496° |
| revolutions per day: | 13.18687888 |
| mean anomaly at epoch: | 281.7849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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