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 58491U 26145.47595441 +.00000000 +00000-0 +15442-3 0 00006
2 58491 43.0009 193.8527 0001726 271.1842 88.8812 15.27585297 07
| Epoch (UTC): | 25 May 2026 11:25:22 |
| Eccentricity: | 0.0001726 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.8527° |
| argument of perigee: | 271.1842° |
| revolutions per day: | 15.27585297 |
| mean anomaly at epoch: | 88.8812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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