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 58723U 26145.61827797 +.00000000 +00000-0 -19286-4 0 00004
2 58723 53.1594 232.5875 0000687 91.9077 268.2003 15.30189912 00
| Epoch (UTC): | 25 May 2026 14:50:19 |
| Eccentricity: | 0.0000687 |
| inclination: | 53.1594° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.5875° |
| argument of perigee: | 91.9077° |
| revolutions per day: | 15.30189912 |
| mean anomaly at epoch: | 268.2003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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