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 59709U 26144.74636874 +.00000000 +00000-0 +24998-4 0 00001
2 59709 53.1576 311.6457 0000901 88.4196 271.6925 15.69704028 06
| Epoch (UTC): | 24 May 2026 17:54:46 |
| Eccentricity: | 0.0000901 |
| inclination: | 53.1576° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 311.6457° |
| argument of perigee: | 88.4196° |
| revolutions per day: | 15.69704028 |
| mean anomaly at epoch: | 271.6925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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