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 58084U 26145.30919887 +.00000000 +00000-0 +63190-3 0 00003
2 58084 43.0012 8.5899 0001201 256.1798 103.8921 15.27603995 09
| Epoch (UTC): | 25 May 2026 07:25:14 |
| Eccentricity: | 0.0001201 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.5899° |
| argument of perigee: | 256.1798° |
| revolutions per day: | 15.27603995 |
| mean anomaly at epoch: | 103.8921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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