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 26075.62591455 +.00000000 +00000-0 +87224-4 0 00002
2 06324 74.0759 301.3528 0008871 331.7101 28.3574 14.45284723 00
| Epoch (UTC): | 16 March 2026 15:01:19 |
| Eccentricity: | 0.0008871 |
| inclination: | 74.0759° |
| perigee height: | 735 km |
| apogee height: | 747 km |
| right ascension of ascending node: | 301.3528° |
| argument of perigee: | 331.7101° |
| revolutions per day: | 14.45284723 |
| mean anomaly at epoch: | 28.3574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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