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 59736U 26145.27476024 +.00000000 +00000-0 +35963-4 0 00003
2 59736 43.0017 110.9163 0001043 273.7915 86.2818 15.27577891 05
| Epoch (UTC): | 25 May 2026 06:35:39 |
| Eccentricity: | 0.0001043 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.9163° |
| argument of perigee: | 273.7915° |
| revolutions per day: | 15.27577891 |
| mean anomaly at epoch: | 86.2818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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