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 62706U 26145.49385882 +.00000000 +00000-0 +60108-3 0 00007
2 62706 97.6975 227.8196 0000756 330.6885 29.4297 15.02364078 01
| Epoch (UTC): | 25 May 2026 11:51:09 |
| Eccentricity: | 0.0000756 |
| inclination: | 97.6975° |
| perigee height: | 559 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 227.8196° |
| argument of perigee: | 330.6885° |
| revolutions per day: | 15.02364078 |
| mean anomaly at epoch: | 29.4297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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