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 50186U 26145.06189181 +.00000000 +00000-0 +46213-4 0 00005
2 50186 53.2148 276.2700 0000829 116.5918 243.5160 15.08834990 07
| Epoch (UTC): | 25 May 2026 01:29:07 |
| Eccentricity: | 0.0000829 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 276.2700° |
| argument of perigee: | 116.5918° |
| revolutions per day: | 15.08834990 |
| mean anomaly at epoch: | 243.5160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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