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 60179U 26145.46132686 +.00000000 +00000-0 +00000-0 0 00000
2 60179 0.0471 116.2332 0001376 320.3699 74.1231 1.00271535 06
| Epoch (UTC): | 25 May 2026 11:04:18 |
| Eccentricity: | 0.0001376 |
| inclination: | 0.0471° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 116.2332° |
| argument of perigee: | 320.3699° |
| revolutions per day: | 1.00271535 |
| mean anomaly at epoch: | 74.1231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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