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 26017.92389115 +.00000000 +00000-0 +62013-4 0 00005
2 15772 71.1064 194.9773 0036256 207.9291 313.6393 14.21962998 04
| Epoch (UTC): | 17 January 2026 22:10:24 |
| Eccentricity: | 0.0036256 |
| inclination: | 71.1064° |
| perigee height: | 793 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 194.9773° |
| argument of perigee: | 207.9291° |
| revolutions per day: | 14.21962998 |
| mean anomaly at epoch: | 313.6393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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