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 62703U 26145.17910146 +.00000000 +00000-0 +10244-3 0 00002
2 62703 97.7027 224.2174 0003649 121.5943 238.5634 14.94105617 00
| Epoch (UTC): | 25 May 2026 04:17:54 |
| Eccentricity: | 0.0003649 |
| inclination: | 97.7027° |
| perigee height: | 583 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 224.2174° |
| argument of perigee: | 121.5943° |
| revolutions per day: | 14.94105617 |
| mean anomaly at epoch: | 238.5634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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