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 58060U 26145.16992492 +.00000000 +00000-0 +12510-3 0 00004
2 58060 43.0027 315.3728 0001469 271.8913 88.1771 15.27588343 05
| Epoch (UTC): | 25 May 2026 04:04:41 |
| Eccentricity: | 0.0001469 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 315.3728° |
| argument of perigee: | 271.8913° |
| revolutions per day: | 15.27588343 |
| mean anomaly at epoch: | 88.1771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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