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 26065.02671080 +.00000000 +00000-0 +53444-4 0 00001
2 00876 65.0577 270.5588 0149830 299.3300 59.2903 14.65671658 06
| Epoch (UTC): | 06 March 2026 00:38:27 |
| Eccentricity: | 0.0149830 |
| inclination: | 65.0577° |
| perigee height: | 569 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 270.5588° |
| argument of perigee: | 299.3300° |
| revolutions per day: | 14.65671658 |
| mean anomaly at epoch: | 59.2903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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