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 60932U 26144.89199779 +.00000000 +00000-0 +76358-5 0 00003
2 60932 53.1593 325.3903 0001072 101.1756 258.9383 15.69708607 01
| Epoch (UTC): | 24 May 2026 21:24:28 |
| Eccentricity: | 0.0001072 |
| inclination: | 53.1593° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 325.3903° |
| argument of perigee: | 101.1756° |
| revolutions per day: | 15.69708607 |
| mean anomaly at epoch: | 258.9383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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