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 06155U 26087.67930588 +.00000000 +00000-0 +19558-3 0 00000
2 06155 35.0009 194.4615 0033367 171.0902 189.0396 14.77739861 07
| Epoch (UTC): | 28 March 2026 16:18:12 |
| Eccentricity: | 0.0033367 |
| inclination: | 35.0009° |
| perigee height: | 613 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 194.4615° |
| argument of perigee: | 171.0902° |
| revolutions per day: | 14.77739861 |
| mean anomaly at epoch: | 189.0396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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