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 26064.96621845 +.00000000 +00000-0 +11214-3 0 00009
2 06324 74.0778 321.1687 0008471 352.9115 7.1922 14.45276566 01
| Epoch (UTC): | 05 March 2026 23:11:21 |
| Eccentricity: | 0.0008471 |
| inclination: | 74.0778° |
| perigee height: | 735 km |
| apogee height: | 747 km |
| right ascension of ascending node: | 321.1687° |
| argument of perigee: | 352.9115° |
| revolutions per day: | 14.45276566 |
| mean anomaly at epoch: | 7.1922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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