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 61575U 26145.36586444 +.00000000 +00000-0 +19361-4 0 00009
2 61575 53.1597 278.2328 0000812 92.8497 267.2614 15.69712083 08
| Epoch (UTC): | 25 May 2026 08:46:50 |
| Eccentricity: | 0.0000812 |
| inclination: | 53.1597° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 278.2328° |
| argument of perigee: | 92.8497° |
| revolutions per day: | 15.69712083 |
| mean anomaly at epoch: | 267.2614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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