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 35688U 26088.09324264 +.00000000 +00000-0 +70603-4 0 00007
2 35688 98.0892 255.5018 0429122 175.5625 300.7790 13.74570607 01
| Epoch (UTC): | 29 March 2026 02:14:16 |
| Eccentricity: | 0.0429122 |
| inclination: | 98.0892° |
| perigee height: | 667 km |
| apogee height: | 1299 km |
| right ascension of ascending node: | 255.5018° |
| argument of perigee: | 175.5625° |
| revolutions per day: | 13.74570607 |
| mean anomaly at epoch: | 300.7790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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