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 11869U 26088.01415843 +.00000000 +00000-0 +56150-4 0 00009
2 11869 74.0473 182.8093 0012797 40.8474 319.3635 14.34630749 07
| Epoch (UTC): | 29 March 2026 00:20:23 |
| Eccentricity: | 0.0012797 |
| inclination: | 74.0473° |
| perigee height: | 767 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 182.8093° |
| argument of perigee: | 40.8474° |
| revolutions per day: | 14.34630749 |
| mean anomaly at epoch: | 319.3635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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