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 26074.61511655 +.00000000 +00000-0 +37113-3 0 00006
2 31598 97.8883 265.6951 0001622 93.5786 266.5620 14.96589596 03
| Epoch (UTC): | 15 March 2026 14:45:46 |
| Eccentricity: | 0.0001622 |
| inclination: | 97.8883° |
| perigee height: | 576 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 265.6951° |
| argument of perigee: | 93.5786° |
| revolutions per day: | 14.96589596 |
| mean anomaly at epoch: | 266.5620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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