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 58597U 26145.31625270 +.00000000 +00000-0 +84640-4 0 00007
2 58597 43.0059 95.7865 0001262 274.3523 85.7185 15.27583843 04
| Epoch (UTC): | 25 May 2026 07:35:24 |
| Eccentricity: | 0.0001262 |
| inclination: | 43.0059° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 95.7865° |
| argument of perigee: | 274.3523° |
| revolutions per day: | 15.27583843 |
| mean anomaly at epoch: | 85.7185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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