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 26075.81859102 +.00000000 +00000-0 +32399-3 0 00002
2 31598 97.8881 266.9085 0001584 91.3236 268.8167 14.96598159 02
| Epoch (UTC): | 16 March 2026 19:38:46 |
| Eccentricity: | 0.0001584 |
| inclination: | 97.8881° |
| perigee height: | 576 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 266.9085° |
| argument of perigee: | 91.3236° |
| revolutions per day: | 14.96598159 |
| mean anomaly at epoch: | 268.8167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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