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 63308U 26145.41260794 +.00000000 +00000-0 +14153-2 0 00000
2 63308 42.9994 162.1158 0000951 337.9603 22.1224 15.70850389 08
| Epoch (UTC): | 25 May 2026 09:54:09 |
| Eccentricity: | 0.0000951 |
| inclination: | 42.9994° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 162.1158° |
| argument of perigee: | 337.9603° |
| revolutions per day: | 15.70850389 |
| mean anomaly at epoch: | 22.1224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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