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 59636U 26145.48281352 +.00000000 +00000-0 +12877-4 0 00002
2 59636 43.0023 66.3688 0000892 265.7273 94.3476 15.27576748 06
| Epoch (UTC): | 25 May 2026 11:35:15 |
| Eccentricity: | 0.0000892 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.3688° |
| argument of perigee: | 265.7273° |
| revolutions per day: | 15.27576748 |
| mean anomaly at epoch: | 94.3476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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