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 59653U 26145.18914985 +.00000000 +00000-0 +31938-3 0 00001
2 59653 43.0025 67.5939 0000816 250.9928 109.0835 15.27550888 08
| Epoch (UTC): | 25 May 2026 04:32:22 |
| Eccentricity: | 0.0000816 |
| inclination: | 43.0025° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 67.5939° |
| argument of perigee: | 250.9928° |
| revolutions per day: | 15.27550888 |
| mean anomaly at epoch: | 109.0835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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