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 63310U 26145.43382970 +.00000000 +00000-0 +13954-2 0 00004
2 63310 43.0009 162.2869 0003766 248.2271 111.8196 15.70844505 09
| Epoch (UTC): | 25 May 2026 10:24:42 |
| Eccentricity: | 0.0003766 |
| inclination: | 43.0009° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 162.2869° |
| argument of perigee: | 248.2271° |
| revolutions per day: | 15.70844505 |
| mean anomaly at epoch: | 111.8196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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