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 58115U 26145.49319991 +.00000000 +00000-0 +29429-4 0 00006
2 58115 53.1597 168.5523 0001033 88.2325 271.8794 15.30195157 02
| Epoch (UTC): | 25 May 2026 11:50:12 |
| Eccentricity: | 0.0001033 |
| inclination: | 53.1597° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.5523° |
| argument of perigee: | 88.2325° |
| revolutions per day: | 15.30195157 |
| mean anomaly at epoch: | 271.8794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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