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 56191U 26145.24378707 +.00000000 +00000-0 +54901-4 0 00004
2 56191 97.2740 33.1646 0004861 105.9286 254.2489 15.27075871 03
| Epoch (UTC): | 25 May 2026 05:51:03 |
| Eccentricity: | 0.0004861 |
| inclination: | 97.2740° |
| perigee height: | 481 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 33.1646° |
| argument of perigee: | 105.9286° |
| revolutions per day: | 15.27075871 |
| mean anomaly at epoch: | 254.2489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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