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 55762U 26145.41827735 +.00000000 +00000-0 +53689-5 0 00009
2 55762 70.0000 31.1068 0002791 268.7515 91.3325 14.98327875 03
| Epoch (UTC): | 25 May 2026 10:02:19 |
| Eccentricity: | 0.0002791 |
| inclination: | 70.0000° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.1068° |
| argument of perigee: | 268.7515° |
| revolutions per day: | 14.98327875 |
| mean anomaly at epoch: | 91.3325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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