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 58092U 26145.02002539 +.00000000 +00000-0 +25120-4 0 00000
2 58092 43.0049 7.3125 0001525 268.1268 91.9409 15.27571024 06
| Epoch (UTC): | 25 May 2026 00:28:50 |
| Eccentricity: | 0.0001525 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 7.3125° |
| argument of perigee: | 268.1268° |
| revolutions per day: | 15.27571024 |
| mean anomaly at epoch: | 91.9409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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