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 63722U 26145.51503880 +.00000000 +00000-0 +43239-3 0 00005
2 63722 53.1578 222.5836 0001768 91.7157 268.4046 15.30207123 05
| Epoch (UTC): | 25 May 2026 12:21:39 |
| Eccentricity: | 0.0001768 |
| inclination: | 53.1578° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.5836° |
| argument of perigee: | 91.7157° |
| revolutions per day: | 15.30207123 |
| mean anomaly at epoch: | 268.4046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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