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 61591U 26145.03624317 +.00000000 +00000-0 +84528-5 0 00001
2 61591 53.1607 55.4181 0000491 85.7317 274.3741 15.33548547 08
| Epoch (UTC): | 25 May 2026 00:52:11 |
| Eccentricity: | 0.0000491 |
| inclination: | 53.1607° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 55.4181° |
| argument of perigee: | 85.7317° |
| revolutions per day: | 15.33548547 |
| mean anomaly at epoch: | 274.3741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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