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 62791U 26145.56693735 +.00000000 +00000-0 +14148-3 0 00001
2 62791 88.9780 86.3252 0012700 224.5015 135.5117 13.51012244 08
| Epoch (UTC): | 25 May 2026 13:36:23 |
| Eccentricity: | 0.0012700 |
| inclination: | 88.9780° |
| perigee height: | 1059 km |
| apogee height: | 1078 km |
| right ascension of ascending node: | 86.3252° |
| argument of perigee: | 224.5015° |
| revolutions per day: | 13.51012244 |
| mean anomaly at epoch: | 135.5117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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