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 17589U 26021.43127113 +.00000000 +00000-0 +17915-3 0 00002
2 17589 70.9193 65.3447 0024388 277.2391 82.5958 14.13048494 01
| Epoch (UTC): | 21 January 2026 10:21:01 |
| Eccentricity: | 0.0024388 |
| inclination: | 70.9193° |
| perigee height: | 831 km |
| apogee height: | 867 km |
| right ascension of ascending node: | 65.3447° |
| argument of perigee: | 277.2391° |
| revolutions per day: | 14.13048494 |
| mean anomaly at epoch: | 82.5958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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