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 58684U 26145.34604905 +.00000000 +00000-0 +12303-4 0 00006
2 58684 43.0052 12.7518 0001238 261.9832 98.0879 15.27577703 01
| Epoch (UTC): | 25 May 2026 08:18:18 |
| Eccentricity: | 0.0001238 |
| inclination: | 43.0052° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.7518° |
| argument of perigee: | 261.9832° |
| revolutions per day: | 15.27577703 |
| mean anomaly at epoch: | 98.0879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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