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 58909U 26145.38546090 +.00000000 +00000-0 +20656-3 0 00009
2 58909 50.0045 99.9248 0011412 336.0058 24.0347 14.83165930 02
| Epoch (UTC): | 25 May 2026 09:15:03 |
| Eccentricity: | 0.0011412 |
| inclination: | 50.0045° |
| perigee height: | 611 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 99.9248° |
| argument of perigee: | 336.0058° |
| revolutions per day: | 14.83165930 |
| mean anomaly at epoch: | 24.0347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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