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 26076.28660714 +.00000000 +00000-0 +28770-3 0 00001
2 31598 97.8881 267.3805 0001568 90.5018 269.6383 14.96600663 01
| Epoch (UTC): | 17 March 2026 06:52:42 |
| Eccentricity: | 0.0001568 |
| inclination: | 97.8881° |
| perigee height: | 576 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 267.3805° |
| argument of perigee: | 90.5018° |
| revolutions per day: | 14.96600663 |
| mean anomaly at epoch: | 269.6383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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