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 58045U 26144.89872838 +.00000000 +00000-0 +37204-4 0 00005
2 58045 53.1613 7.3662 0001195 77.8092 282.3042 15.30195389 01
| Epoch (UTC): | 24 May 2026 21:34:10 |
| Eccentricity: | 0.0001195 |
| inclination: | 53.1613° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 7.3662° |
| argument of perigee: | 77.8092° |
| revolutions per day: | 15.30195389 |
| mean anomaly at epoch: | 282.3042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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