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 60104U 26145.11683928 +.00000000 +00000-0 +35667-5 0 00002
2 60104 53.1608 42.3966 0001349 92.0121 268.1034 15.30200077 07
| Epoch (UTC): | 25 May 2026 02:48:14 |
| Eccentricity: | 0.0001349 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 42.3966° |
| argument of perigee: | 92.0121° |
| revolutions per day: | 15.30200077 |
| mean anomaly at epoch: | 268.1034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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