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 62904U 26145.66578413 +.00000000 +00000-0 +14409-3 0 00003
2 62904 81.9949 97.4755 0011231 124.9687 235.2589 14.94921627 04
| Epoch (UTC): | 25 May 2026 15:58:43 |
| Eccentricity: | 0.0011231 |
| inclination: | 81.9949° |
| perigee height: | 575 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 97.4755° |
| argument of perigee: | 124.9687° |
| revolutions per day: | 14.94921627 |
| mean anomaly at epoch: | 235.2589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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