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 19548U 26150.42208977 +.00000000 +00000-0 +00000-0 0 00003
2 19548 12.6156 341.1225 0039238 356.7275 12.9243 1.00281048 03
| Epoch (UTC): | 30 May 2026 10:07:48 |
| Eccentricity: | 0.0039238 |
| inclination: | 12.6156° |
| perigee height: | 35619 km |
| apogee height: | 35949 km |
| right ascension of ascending node: | 341.1225° |
| argument of perigee: | 356.7275° |
| revolutions per day: | 1.00281048 |
| mean anomaly at epoch: | 12.9243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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