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 59124U 26145.58613998 +.00000000 +00000-0 +14044-3 0 00007
2 59124 97.5581 281.6375 0009865 334.3688 25.7061 15.28465712 05
| Epoch (UTC): | 25 May 2026 14:04:02 |
| Eccentricity: | 0.0009865 |
| inclination: | 97.5581° |
| perigee height: | 474 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 281.6375° |
| argument of perigee: | 334.3688° |
| revolutions per day: | 15.28465712 |
| mean anomaly at epoch: | 25.7061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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