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 59924U 26145.53877029 +.00000000 +00000-0 +50659-4 0 00000
2 59924 43.0027 244.0101 0001697 266.3043 93.7615 15.27582684 05
| Epoch (UTC): | 25 May 2026 12:55:49 |
| Eccentricity: | 0.0001697 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 244.0101° |
| argument of perigee: | 266.3043° |
| revolutions per day: | 15.27582684 |
| mean anomaly at epoch: | 93.7615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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