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 58528U 26145.39369063 +.00000000 +00000-0 +63437-4 0 00005
2 58528 43.0030 30.1231 0000884 271.3021 88.7729 15.27577969 05
| Epoch (UTC): | 25 May 2026 09:26:54 |
| Eccentricity: | 0.0000884 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 30.1231° |
| argument of perigee: | 271.3021° |
| revolutions per day: | 15.27577969 |
| mean anomaly at epoch: | 88.7729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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