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 50179U 26145.33145027 +.00000000 +00000-0 -47813-5 0 00007
2 50179 53.2160 265.0623 0000778 82.9702 277.1378 15.08834674 06
| Epoch (UTC): | 25 May 2026 07:57:17 |
| Eccentricity: | 0.0000778 |
| inclination: | 53.2160° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 265.0623° |
| argument of perigee: | 82.9702° |
| revolutions per day: | 15.08834674 |
| mean anomaly at epoch: | 277.1378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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