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 62619U 26145.18379736 +.00000000 +00000-0 +20773-3 0 00001
2 62619 97.4046 226.2086 0007675 55.0949 305.1010 15.26704684 02
| Epoch (UTC): | 25 May 2026 04:24:40 |
| Eccentricity: | 0.0007675 |
| inclination: | 97.4046° |
| perigee height: | 480 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 226.2086° |
| argument of perigee: | 55.0949° |
| revolutions per day: | 15.26704684 |
| mean anomaly at epoch: | 305.1010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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