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 15772U 26071.45534860 +.00000000 +00000-0 +93673-4 0 00008
2 15772 71.1063 81.8850 0033115 123.5864 28.0577 14.21983223 08
| Epoch (UTC): | 12 March 2026 10:55:42 |
| Eccentricity: | 0.0033115 |
| inclination: | 71.1063° |
| perigee height: | 795 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 81.8850° |
| argument of perigee: | 123.5864° |
| revolutions per day: | 14.21983223 |
| mean anomaly at epoch: | 28.0577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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