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 58523U 26145.38341300 +.00000000 +00000-0 -43412-4 0 00005
2 58523 43.0038 30.0498 0001090 272.1136 87.9591 15.27570720 04
| Epoch (UTC): | 25 May 2026 09:12:06 |
| Eccentricity: | 0.0001090 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 30.0498° |
| argument of perigee: | 272.1136° |
| revolutions per day: | 15.27570720 |
| mean anomaly at epoch: | 87.9591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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