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 58137U 26145.18112235 +.00000000 +00000-0 +71965-4 0 00000
2 58137 43.0026 60.6564 0001407 267.2073 92.8617 15.27578406 05
| Epoch (UTC): | 25 May 2026 04:20:48 |
| Eccentricity: | 0.0001407 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 60.6564° |
| argument of perigee: | 267.2073° |
| revolutions per day: | 15.27578406 |
| mean anomaly at epoch: | 92.8617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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