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 58237U 26145.18000164 +.00000000 +00000-0 +62353-4 0 00009
2 58237 43.0044 213.1687 0001953 272.8609 87.2019 15.27575783 09
| Epoch (UTC): | 25 May 2026 04:19:12 |
| Eccentricity: | 0.0001953 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 213.1687° |
| argument of perigee: | 272.8609° |
| revolutions per day: | 15.27575783 |
| mean anomaly at epoch: | 87.2019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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