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 63412U 26145.39914164 +.00000000 +00000-0 +68818-3 0 00008
2 63412 43.0016 37.0824 0001571 273.5711 86.4961 15.27602961 09
| Epoch (UTC): | 25 May 2026 09:34:45 |
| Eccentricity: | 0.0001571 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.0824° |
| argument of perigee: | 273.5711° |
| revolutions per day: | 15.27602961 |
| mean anomaly at epoch: | 86.4961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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