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 58469U 26145.61267455 +.00000000 +00000-0 +20798-3 0 00008
2 58469 97.5756 233.7969 0009624 169.9418 190.2018 15.32684666 09
| Epoch (UTC): | 25 May 2026 14:42:15 |
| Eccentricity: | 0.0009624 |
| inclination: | 97.5756° |
| perigee height: | 461 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 233.7969° |
| argument of perigee: | 169.9418° |
| revolutions per day: | 15.32684666 |
| mean anomaly at epoch: | 190.2018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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