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 62392U 26145.17119311 +.00000000 +00000-0 +23387-3 0 00003
2 62392 45.0012 59.0021 0002049 204.1988 155.8800 15.28738672 06
| Epoch (UTC): | 25 May 2026 04:06:31 |
| Eccentricity: | 0.0002049 |
| inclination: | 45.0012° |
| perigee height: | 478 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 59.0021° |
| argument of perigee: | 204.1988° |
| revolutions per day: | 15.28738672 |
| mean anomaly at epoch: | 155.8800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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