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 58897U 26145.50734352 +.00000000 +00000-0 +15376-4 0 00003
2 58897 53.1614 325.5075 0001302 86.3732 273.7418 15.31704006 00
| Epoch (UTC): | 25 May 2026 12:10:34 |
| Eccentricity: | 0.0001302 |
| inclination: | 53.1614° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 325.5075° |
| argument of perigee: | 86.3732° |
| revolutions per day: | 15.31704006 |
| mean anomaly at epoch: | 273.7418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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