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 58446U 26145.23727432 +.00000000 +00000-0 +41471-4 0 00009
2 58446 43.0040 329.1101 0001399 286.4375 73.6323 15.27578761 07
| Epoch (UTC): | 25 May 2026 05:41:40 |
| Eccentricity: | 0.0001399 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 329.1101° |
| argument of perigee: | 286.4375° |
| revolutions per day: | 15.27578761 |
| mean anomaly at epoch: | 73.6323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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