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 58280U 26145.58043207 +.00000000 +00000-0 +41541-3 0 00001
2 58280 97.3882 236.0550 0005276 208.8443 151.2519 15.53373694 02
| Epoch (UTC): | 25 May 2026 13:55:49 |
| Eccentricity: | 0.0005276 |
| inclination: | 97.3882° |
| perigee height: | 403 km |
| apogee height: | 410 km |
| right ascension of ascending node: | 236.0550° |
| argument of perigee: | 208.8443° |
| revolutions per day: | 15.53373694 |
| mean anomaly at epoch: | 151.2519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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