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 62179U 26145.25083187 +.00000000 +00000-0 +23440-3 0 00006
2 62179 70.0017 331.3328 0002021 272.3192 87.7736 14.98335924 02
| Epoch (UTC): | 25 May 2026 06:01:11 |
| Eccentricity: | 0.0002021 |
| inclination: | 70.0017° |
| perigee height: | 571 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 331.3328° |
| argument of perigee: | 272.3192° |
| revolutions per day: | 14.98335924 |
| mean anomaly at epoch: | 87.7736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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