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 26017.22264957 +.00000000 +00000-0 +46222-4 0 00008
2 15772 71.1064 196.4589 0036299 209.0143 323.9438 14.21962775 09
| Epoch (UTC): | 17 January 2026 05:20:36 |
| Eccentricity: | 0.0036299 |
| inclination: | 71.1064° |
| perigee height: | 793 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 196.4589° |
| argument of perigee: | 209.0143° |
| revolutions per day: | 14.21962775 |
| mean anomaly at epoch: | 323.9438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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