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 58180U 26145.15146140 +.00000000 +00000-0 +14560-2 0 00003
2 58180 43.0014 71.1711 0002129 203.9411 156.1343 15.30064629 07
| Epoch (UTC): | 25 May 2026 03:38:06 |
| Eccentricity: | 0.0002129 |
| inclination: | 43.0014° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 71.1711° |
| argument of perigee: | 203.9411° |
| revolutions per day: | 15.30064629 |
| mean anomaly at epoch: | 156.1343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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