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 04579U 26088.19868208 +.00000000 +00000-0 +14858-3 0 00003
2 04579 74.0006 68.5797 0009796 0.5653 359.5523 14.63618832 00
| Epoch (UTC): | 29 March 2026 04:46:06 |
| Eccentricity: | 0.0009796 |
| inclination: | 74.0006° |
| perigee height: | 675 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 68.5797° |
| argument of perigee: | 0.5653° |
| revolutions per day: | 14.63618832 |
| mean anomaly at epoch: | 359.5523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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