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 62646U 26145.48465247 +.00000000 +00000-0 +37419-3 0 00002
2 62646 97.4014 227.6758 0002759 65.6536 294.4991 15.28927213 00
| Epoch (UTC): | 25 May 2026 11:37:53 |
| Eccentricity: | 0.0002759 |
| inclination: | 97.4014° |
| perigee height: | 477 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 227.6758° |
| argument of perigee: | 65.6536° |
| revolutions per day: | 15.28927213 |
| mean anomaly at epoch: | 294.4991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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