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 58968U 26145.63582418 +.00000000 +00000-0 +77311-4 0 00007
2 58968 53.1606 271.4342 0000483 7.3893 352.7115 15.30197688 09
| Epoch (UTC): | 25 May 2026 15:15:35 |
| Eccentricity: | 0.0000483 |
| inclination: | 53.1606° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 271.4342° |
| argument of perigee: | 7.3893° |
| revolutions per day: | 15.30197688 |
| mean anomaly at epoch: | 352.7115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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