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 58605U 26145.12702056 +.00000000 +00000-0 +15083-2 0 00007
2 58605 43.0001 96.0801 0004867 171.1399 188.9541 15.32225300 03
| Epoch (UTC): | 25 May 2026 03:02:54 |
| Eccentricity: | 0.0004867 |
| inclination: | 43.0001° |
| perigee height: | 466 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 96.0801° |
| argument of perigee: | 171.1399° |
| revolutions per day: | 15.32225300 |
| mean anomaly at epoch: | 188.9541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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