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 58393U 26145.63223559 +.00000000 +00000-0 +80376-4 0 00002
2 58393 53.1627 2.8332 0001221 94.0123 266.1019 15.34384938 00
| Epoch (UTC): | 25 May 2026 15:10:25 |
| Eccentricity: | 0.0001221 |
| inclination: | 53.1627° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 2.8332° |
| argument of perigee: | 94.0123° |
| revolutions per day: | 15.34384938 |
| mean anomaly at epoch: | 266.1019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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