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 43619U 26088.20287066 +.00000000 +00000-0 +11371-3 0 00007
2 43619 97.5192 323.7521 0001891 79.2537 280.8898 14.96192529 04
| Epoch (UTC): | 29 March 2026 04:52:08 |
| Eccentricity: | 0.0001891 |
| inclination: | 97.5192° |
| perigee height: | 577 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 323.7521° |
| argument of perigee: | 79.2537° |
| revolutions per day: | 14.96192529 |
| mean anomaly at epoch: | 280.8898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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