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 59165U 26144.97398735 +.00000000 +00000-0 -11391-4 0 00007
2 59165 43.0035 36.0974 0001204 265.5661 94.5053 15.27581594 03
| Epoch (UTC): | 24 May 2026 23:22:32 |
| Eccentricity: | 0.0001204 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 36.0974° |
| argument of perigee: | 265.5661° |
| revolutions per day: | 15.27581594 |
| mean anomaly at epoch: | 94.5053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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