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 11605U 26088.07887507 +.00000000 +00000-0 +12519-3 0 00003
2 11605 81.2093 309.3246 0011247 137.8713 222.3323 14.07465089 01
| Epoch (UTC): | 29 March 2026 01:53:34 |
| Eccentricity: | 0.0011247 |
| inclination: | 81.2093° |
| perigee height: | 860 km |
| apogee height: | 876 km |
| right ascension of ascending node: | 309.3246° |
| argument of perigee: | 137.8713° |
| revolutions per day: | 14.07465089 |
| mean anomaly at epoch: | 222.3323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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