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 26065.45075152 +.00000000 +00000-0 +12675-3 0 00000
2 06324 74.0777 320.2680 0008500 351.8906 8.2114 14.45277250 08
| Epoch (UTC): | 06 March 2026 10:49:04 |
| Eccentricity: | 0.0008500 |
| inclination: | 74.0777° |
| perigee height: | 735 km |
| apogee height: | 747 km |
| right ascension of ascending node: | 320.2680° |
| argument of perigee: | 351.8906° |
| revolutions per day: | 14.45277250 |
| mean anomaly at epoch: | 8.2114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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