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 00876U 26074.16992541 +.00000000 +00000-0 +53792-4 0 00000
2 00876 65.0580 243.5393 0150316 296.0807 62.4889 14.65678924 03
| Epoch (UTC): | 15 March 2026 04:04:41 |
| Eccentricity: | 0.0150316 |
| inclination: | 65.0580° |
| perigee height: | 569 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 243.5393° |
| argument of perigee: | 296.0807° |
| revolutions per day: | 14.65678924 |
| mean anomaly at epoch: | 62.4889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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