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 62647U 26145.17757825 +.00000000 +00000-0 +13436-2 0 00007
2 62647 97.3935 226.8971 0001298 107.0041 253.1343 15.30607212 09
| Epoch (UTC): | 25 May 2026 04:15:42 |
| Eccentricity: | 0.0001298 |
| inclination: | 97.3935° |
| perigee height: | 473 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 226.8971° |
| argument of perigee: | 107.0041° |
| revolutions per day: | 15.30607212 |
| mean anomaly at epoch: | 253.1343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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