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 62599U 26145.04822115 +.00000000 +00000-0 +10411-2 0 00004
2 62599 43.0016 25.8796 0002732 264.1795 95.8762 15.70894005 08
| Epoch (UTC): | 25 May 2026 01:09:26 |
| Eccentricity: | 0.0002732 |
| inclination: | 43.0016° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 25.8796° |
| argument of perigee: | 264.1795° |
| revolutions per day: | 15.70894005 |
| mean anomaly at epoch: | 95.8762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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