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 58967U 26145.41411181 +.00000000 +00000-0 +70871-4 0 00004
2 58967 53.1609 300.0614 0001085 98.0555 262.0569 15.30194851 08
| Epoch (UTC): | 25 May 2026 09:56:19 |
| Eccentricity: | 0.0001085 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.0614° |
| argument of perigee: | 98.0555° |
| revolutions per day: | 15.30194851 |
| mean anomaly at epoch: | 262.0569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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