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 26066.94895667 +.00000000 +00000-0 -55978-4 0 00006
2 17589 70.9228 329.6772 0024358 216.9669 142.9775 14.13055261 00
| Epoch (UTC): | 07 March 2026 22:46:29 |
| Eccentricity: | 0.0024358 |
| inclination: | 70.9228° |
| perigee height: | 831 km |
| apogee height: | 867 km |
| right ascension of ascending node: | 329.6772° |
| argument of perigee: | 216.9669° |
| revolutions per day: | 14.13055261 |
| mean anomaly at epoch: | 142.9775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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