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 63190U 26145.60594292 +.00000000 +00000-0 +16020-2 0 00008
2 63190 43.0021 216.6687 0001917 301.7291 58.3390 15.70881947 06
| Epoch (UTC): | 25 May 2026 14:32:33 |
| Eccentricity: | 0.0001917 |
| inclination: | 43.0021° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 216.6687° |
| argument of perigee: | 301.7291° |
| revolutions per day: | 15.70881947 |
| mean anomaly at epoch: | 58.3390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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