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 59903U 26145.14993139 +.00000000 +00000-0 +28763-4 0 00006
2 59903 43.0030 53.3045 0001213 270.3609 89.7104 15.27584273 05
| Epoch (UTC): | 25 May 2026 03:35:54 |
| Eccentricity: | 0.0001213 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 53.3045° |
| argument of perigee: | 270.3609° |
| revolutions per day: | 15.27584273 |
| mean anomaly at epoch: | 89.7104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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