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 26020.93980781 +.00000000 +00000-0 +15028-3 0 00009
2 15772 71.1066 188.6058 0036074 203.3569 272.2068 14.21965022 08
| Epoch (UTC): | 20 January 2026 22:33:19 |
| Eccentricity: | 0.0036074 |
| inclination: | 71.1066° |
| perigee height: | 793 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 188.6058° |
| argument of perigee: | 203.3569° |
| revolutions per day: | 14.21965022 |
| mean anomaly at epoch: | 272.2068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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