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 58163U 26145.46398598 +.00000000 +00000-0 +34771-4 0 00002
2 58163 53.1595 210.4314 0001007 79.3403 280.7711 15.30192395 06
| Epoch (UTC): | 25 May 2026 11:08:08 |
| Eccentricity: | 0.0001007 |
| inclination: | 53.1595° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.4314° |
| argument of perigee: | 79.3403° |
| revolutions per day: | 15.30192395 |
| mean anomaly at epoch: | 280.7711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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