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 26064.76620433 +.00000000 +00000-0 +11557-3 0 00009
2 06153 35.0064 319.6697 0006095 133.4673 269.7059 14.59994443 03
| Epoch (UTC): | 05 March 2026 18:23:20 |
| Eccentricity: | 0.0006095 |
| inclination: | 35.0064° |
| perigee height: | 689 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 319.6697° |
| argument of perigee: | 133.4673° |
| revolutions per day: | 14.59994443 |
| mean anomaly at epoch: | 269.7059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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