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 58356U 26145.41668949 +.00000000 +00000-0 +54165-4 0 00000
2 58356 43.0065 277.1058 0002139 271.8995 88.1612 15.27574161 08
| Epoch (UTC): | 25 May 2026 10:00:01 |
| Eccentricity: | 0.0002139 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 277.1058° |
| argument of perigee: | 271.8995° |
| revolutions per day: | 15.27574161 |
| mean anomaly at epoch: | 88.1612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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