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 59757U 26145.35854669 +.00000000 +00000-0 +69735-5 0 00005
2 59757 53.1601 188.4399 0001073 72.3855 287.7280 15.69707220 07
| Epoch (UTC): | 25 May 2026 08:36:18 |
| Eccentricity: | 0.0001073 |
| inclination: | 53.1601° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 188.4399° |
| argument of perigee: | 72.3855° |
| revolutions per day: | 15.69707220 |
| mean anomaly at epoch: | 287.7280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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