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 25544U 26101.48935997 +.00000000 +00000-0 +11816-3 0 00007
2 25544 51.6326 270.1822 0006432 299.5706 60.4641 15.48873216 06
| Epoch (UTC): | 11 April 2026 11:44:40 |
| Eccentricity: | 0.0006432 |
| inclination: | 51.6326° |
| perigee height: | 416 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 270.1822° |
| argument of perigee: | 299.5706° |
| revolutions per day: | 15.48873216 |
| mean anomaly at epoch: | 60.4641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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