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 61558U 26145.55360795 +.00000000 +00000-0 +23788-3 0 00007
2 61558 88.9834 59.6374 0010824 166.3313 193.8164 14.06056390 05
| Epoch (UTC): | 25 May 2026 13:17:11 |
| Eccentricity: | 0.0010824 |
| inclination: | 88.9834° |
| perigee height: | 865 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 59.6374° |
| argument of perigee: | 166.3313° |
| revolutions per day: | 14.06056390 |
| mean anomaly at epoch: | 193.8164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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