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 63063U 26145.24096426 +.00000000 +00000-0 +15377-2 0 00007
2 63063 42.9976 273.6211 0001522 293.9015 66.1693 15.70877535 07
| Epoch (UTC): | 25 May 2026 05:46:59 |
| Eccentricity: | 0.0001522 |
| inclination: | 42.9976° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 273.6211° |
| argument of perigee: | 293.9015° |
| revolutions per day: | 15.70877535 |
| mean anomaly at epoch: | 66.1693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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