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 26021.49174659 +.00000000 +00000-0 +14230-3 0 00004
2 15772 71.1066 187.4397 0036046 202.5234 217.5980 14.21965315 00
| Epoch (UTC): | 21 January 2026 11:48:06 |
| Eccentricity: | 0.0036046 |
| inclination: | 71.1066° |
| perigee height: | 793 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 187.4397° |
| argument of perigee: | 202.5234° |
| revolutions per day: | 14.21965315 |
| mean anomaly at epoch: | 217.5980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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