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 29709U 26078.89400837 +.00000000 +00000-0 +10722-3 0 00007
2 29709 98.1335 76.1173 0013485 113.2813 246.9823 14.85847509 08
| Epoch (UTC): | 19 March 2026 21:27:22 |
| Eccentricity: | 0.0013485 |
| inclination: | 98.1335° |
| perigee height: | 602 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 76.1173° |
| argument of perigee: | 113.2813° |
| revolutions per day: | 14.85847509 |
| mean anomaly at epoch: | 246.9823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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