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 06324U 26100.12914722 +.00000000 +00000-0 +10802-3 0 00009
2 06324 74.0748 255.7939 0009532 284.7267 75.2834 14.45305650 04
| Epoch (UTC): | 10 April 2026 03:05:58 |
| Eccentricity: | 0.0009532 |
| inclination: | 74.0748° |
| perigee height: | 734 km |
| apogee height: | 748 km |
| right ascension of ascending node: | 255.7939° |
| argument of perigee: | 284.7267° |
| revolutions per day: | 14.45305650 |
| mean anomaly at epoch: | 75.2834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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