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 57832U 26145.62529264 +.00000000 +00000-0 +75935-4 0 00005
2 57832 85.9898 270.0562 0001776 101.5816 258.5566 14.12442999 01
| Epoch (UTC): | 25 May 2026 15:00:25 |
| Eccentricity: | 0.0001776 |
| inclination: | 85.9898° |
| perigee height: | 850 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 270.0562° |
| argument of perigee: | 101.5816° |
| revolutions per day: | 14.12442999 |
| mean anomaly at epoch: | 258.5566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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