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 63405U 26145.40478147 +.00000000 +00000-0 +11081-2 0 00007
2 63405 43.0049 33.7332 0002326 265.8100 94.2486 15.27609542 00
| Epoch (UTC): | 25 May 2026 09:42:53 |
| Eccentricity: | 0.0002326 |
| inclination: | 43.0049° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 33.7332° |
| argument of perigee: | 265.8100° |
| revolutions per day: | 15.27609542 |
| mean anomaly at epoch: | 94.2486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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