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 31598U 26073.27791373 +.00000000 +00000-0 +43212-3 0 00001
2 31598 97.8882 264.3467 0001589 95.2068 264.9334 14.96577744 00
| Epoch (UTC): | 14 March 2026 06:40:11 |
| Eccentricity: | 0.0001589 |
| inclination: | 97.8882° |
| perigee height: | 576 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 264.3467° |
| argument of perigee: | 95.2068° |
| revolutions per day: | 14.96577744 |
| mean anomaly at epoch: | 264.9334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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