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 58274U 26145.50959073 +.00000000 +00000-0 +49196-3 0 00007
2 58274 97.3846 237.1119 0006991 208.8149 151.2721 15.56096218 08
| Epoch (UTC): | 25 May 2026 12:13:48 |
| Eccentricity: | 0.0006991 |
| inclination: | 97.3846° |
| perigee height: | 394 km |
| apogee height: | 404 km |
| right ascension of ascending node: | 237.1119° |
| argument of perigee: | 208.8149° |
| revolutions per day: | 15.56096218 |
| mean anomaly at epoch: | 151.2721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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