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 60933U 26145.20543728 +.00000000 +00000-0 +24108-4 0 00002
2 60933 53.1576 323.7896 0000899 55.2090 304.9013 15.69714777 09
| Epoch (UTC): | 25 May 2026 04:55:49 |
| Eccentricity: | 0.0000899 |
| inclination: | 53.1576° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 323.7896° |
| argument of perigee: | 55.2090° |
| revolutions per day: | 15.69714777 |
| mean anomaly at epoch: | 304.9013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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