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 58521U 26145.37570213 +.00000000 +00000-0 +87086-3 0 00002
2 58521 43.0085 29.9965 0000777 259.6535 100.4229 15.27591688 09
| Epoch (UTC): | 25 May 2026 09:01:00 |
| Eccentricity: | 0.0000777 |
| inclination: | 43.0085° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 29.9965° |
| argument of perigee: | 259.6535° |
| revolutions per day: | 15.27591688 |
| mean anomaly at epoch: | 100.4229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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