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 60599U 26145.47421304 +.00000000 +00000-0 +41165-4 0 00006
2 60599 53.1614 310.6379 0001144 82.8297 277.2834 15.30196979 09
| Epoch (UTC): | 25 May 2026 11:22:52 |
| Eccentricity: | 0.0001144 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.6379° |
| argument of perigee: | 82.8297° |
| revolutions per day: | 15.30196979 |
| mean anomaly at epoch: | 277.2834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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