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 58477U 26145.22819872 +.00000000 +00000-0 +49723-4 0 00000
2 58477 43.0045 339.9429 0001375 264.8593 95.2102 15.27581880 05
| Epoch (UTC): | 25 May 2026 05:28:36 |
| Eccentricity: | 0.0001375 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 339.9429° |
| argument of perigee: | 264.8593° |
| revolutions per day: | 15.27581880 |
| mean anomaly at epoch: | 95.2102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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