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 59588U 26143.21817437 +.00000000 +00000-0 +23650-2 0 00005
2 59588 97.1747 67.5928 0022166 22.8878 337.3271 13.92695105 08
| Epoch (UTC): | 23 May 2026 05:14:10 |
| Eccentricity: | 0.0022166 |
| inclination: | 97.1747° |
| perigee height: | 903 km |
| apogee height: | 935 km |
| right ascension of ascending node: | 67.5928° |
| argument of perigee: | 22.8878° |
| revolutions per day: | 13.92695105 |
| mean anomaly at epoch: | 337.3271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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