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 58070U 26143.97498252 +.00000000 +00000-0 +27515-3 0 00008
2 58070 43.0019 321.8941 0001530 266.7027 93.3649 15.27595494 01
| Epoch (UTC): | 23 May 2026 23:23:58 |
| Eccentricity: | 0.0001530 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 321.8941° |
| argument of perigee: | 266.7027° |
| revolutions per day: | 15.27595494 |
| mean anomaly at epoch: | 93.3649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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