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 58863U 26145.55885072 +.00000000 +00000-0 +44464-4 0 00007
2 58863 43.0007 174.3712 0001165 272.5572 87.5146 15.27578856 09
| Epoch (UTC): | 25 May 2026 13:24:44 |
| Eccentricity: | 0.0001165 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.3712° |
| argument of perigee: | 272.5572° |
| revolutions per day: | 15.27578856 |
| mean anomaly at epoch: | 87.5146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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