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 58559U 26145.61598700 +.00000000 +00000-0 +25147-3 0 00001
2 58559 34.9916 221.9901 0013092 200.6027 159.4159 15.17386894 08
| Epoch (UTC): | 25 May 2026 14:47:01 |
| Eccentricity: | 0.0013092 |
| inclination: | 34.9916° |
| perigee height: | 505 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 221.9901° |
| argument of perigee: | 200.6027° |
| revolutions per day: | 15.17386894 |
| mean anomaly at epoch: | 159.4159° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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