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 63407U 26145.39707368 +.00000000 +00000-0 +61900-3 0 00003
2 63407 42.9971 33.6706 0000530 273.9225 86.1566 15.27581111 01
| Epoch (UTC): | 25 May 2026 09:31:47 |
| Eccentricity: | 0.0000530 |
| inclination: | 42.9971° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 33.6706° |
| argument of perigee: | 273.9225° |
| revolutions per day: | 15.27581111 |
| mean anomaly at epoch: | 86.1566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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