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 36509U 26088.16612139 +.00000000 +00000-0 +16146-4 0 00001
2 36509 91.9229 62.5759 0275499 124.9810 237.7567 13.93847222 00
| Epoch (UTC): | 29 March 2026 03:59:12 |
| Eccentricity: | 0.0275499 |
| inclination: | 91.9229° |
| perigee height: | 714 km |
| apogee height: | 1116 km |
| right ascension of ascending node: | 62.5759° |
| argument of perigee: | 124.9810° |
| revolutions per day: | 13.93847222 |
| mean anomaly at epoch: | 237.7567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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