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 26067.87341432 +.00000000 +00000-0 +11523-3 0 00006
2 06324 74.0774 315.7648 0008599 347.0231 13.0705 14.45279227 00
| Epoch (UTC): | 08 March 2026 20:57:42 |
| Eccentricity: | 0.0008599 |
| inclination: | 74.0774° |
| perigee height: | 735 km |
| apogee height: | 747 km |
| right ascension of ascending node: | 315.7648° |
| argument of perigee: | 347.0231° |
| revolutions per day: | 14.45279227 |
| mean anomaly at epoch: | 13.0705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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