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 65636U 26144.87334912 +.00000000 +00000-0 +77802-3 0 00000
2 65636 53.1604 312.6148 0000498 63.2841 296.8213 15.34416824 06
| Epoch (UTC): | 24 May 2026 20:57:37 |
| Eccentricity: | 0.0000498 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 312.6148° |
| argument of perigee: | 63.2841° |
| revolutions per day: | 15.34416824 |
| mean anomaly at epoch: | 296.8213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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