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 58362U 26145.42440572 +.00000000 +00000-0 -16434-5 0 00007
2 58362 43.0048 277.1941 0001414 264.8824 95.1866 15.27573394 01
| Epoch (UTC): | 25 May 2026 10:11:08 |
| Eccentricity: | 0.0001414 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.1941° |
| argument of perigee: | 264.8824° |
| revolutions per day: | 15.27573394 |
| mean anomaly at epoch: | 95.1866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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