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 62951U 26145.61596594 +.00000000 +00000-0 +70364-3 0 00002
2 62951 53.1591 232.4286 0000685 103.2008 256.9071 15.34418555 00
| Epoch (UTC): | 25 May 2026 14:46:59 |
| Eccentricity: | 0.0000685 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 232.4286° |
| argument of perigee: | 103.2008° |
| revolutions per day: | 15.34418555 |
| mean anomaly at epoch: | 256.9071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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