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 06153U 26087.69562235 +.00000000 +00000-0 +74323-4 0 00002
2 06153 35.0049 189.0282 0007143 312.8882 195.3271 14.60012766 06
| Epoch (UTC): | 28 March 2026 16:41:41 |
| Eccentricity: | 0.0007143 |
| inclination: | 35.0049° |
| perigee height: | 688 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 189.0282° |
| argument of perigee: | 312.8882° |
| revolutions per day: | 14.60012766 |
| mean anomaly at epoch: | 195.3271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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