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 59555U 26144.75744833 +.00000000 +00000-0 -24494-4 0 00008
2 59555 43.0000 274.2968 0001068 262.8184 97.2546 15.27572563 08
| Epoch (UTC): | 24 May 2026 18:10:43 |
| Eccentricity: | 0.0001068 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 274.2968° |
| argument of perigee: | 262.8184° |
| revolutions per day: | 15.27572563 |
| mean anomaly at epoch: | 97.2546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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