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 15755U 26071.53036402 +.00000000 +00000-0 +64937-4 0 00008
2 15755 71.1105 119.9714 0033503 137.3704 223.0032 14.20990648 06
| Epoch (UTC): | 12 March 2026 12:43:43 |
| Eccentricity: | 0.0033503 |
| inclination: | 71.1105° |
| perigee height: | 798 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 119.9714° |
| argument of perigee: | 137.3704° |
| revolutions per day: | 14.20990648 |
| mean anomaly at epoch: | 223.0032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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