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 58747U 26145.46640829 +.00000000 +00000-0 +37005-4 0 00000
2 58747 43.0029 146.3401 0002040 274.7102 85.3517 15.27580933 01
| Epoch (UTC): | 25 May 2026 11:11:37 |
| Eccentricity: | 0.0002040 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.3401° |
| argument of perigee: | 274.7102° |
| revolutions per day: | 15.27580933 |
| mean anomaly at epoch: | 85.3517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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