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 63108U 26145.36940817 +.00000000 +00000-0 +13697-2 0 00005
2 63108 43.0041 134.7836 0002700 260.9384 99.1179 15.70900055 03
| Epoch (UTC): | 25 May 2026 08:51:56 |
| Eccentricity: | 0.0002700 |
| inclination: | 43.0041° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 134.7836° |
| argument of perigee: | 260.9384° |
| revolutions per day: | 15.70900055 |
| mean anomaly at epoch: | 99.1179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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