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 15598U 26017.70156917 +.00000000 +00000-0 +55706-4 0 00000
2 15598 82.9388 295.4693 0021768 340.1204 86.1054 13.76819468 01
| Epoch (UTC): | 17 January 2026 16:50:15 |
| Eccentricity: | 0.0021768 |
| inclination: | 82.9388° |
| perigee height: | 959 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 295.4693° |
| argument of perigee: | 340.1204° |
| revolutions per day: | 13.76819468 |
| mean anomaly at epoch: | 86.1054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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