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 55763U 26145.46021591 +.00000000 +00000-0 -30989-4 0 00009
2 55763 70.0004 50.7327 0002793 267.8049 92.2790 14.98327415 03
| Epoch (UTC): | 25 May 2026 11:02:42 |
| Eccentricity: | 0.0002793 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 50.7327° |
| argument of perigee: | 267.8049° |
| revolutions per day: | 14.98327415 |
| mean anomaly at epoch: | 92.2790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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