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 58716U 26144.96196567 +.00000000 +00000-0 +25135-4 0 00006
2 58716 53.1616 235.6073 0001244 96.3202 263.7941 15.30192513 02
| Epoch (UTC): | 24 May 2026 23:05:13 |
| Eccentricity: | 0.0001244 |
| inclination: | 53.1616° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.6073° |
| argument of perigee: | 96.3202° |
| revolutions per day: | 15.30192513 |
| mean anomaly at epoch: | 263.7941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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