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 55658U 26144.99220125 +.00000000 +00000-0 +23744-4 0 00003
2 55658 69.9994 351.9551 0002902 268.6069 91.4757 14.98330710 05
| Epoch (UTC): | 24 May 2026 23:48:46 |
| Eccentricity: | 0.0002902 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 351.9551° |
| argument of perigee: | 268.6069° |
| revolutions per day: | 14.98330710 |
| mean anomaly at epoch: | 91.4757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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