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 22577U 26100.07938750 +.00000000 +00000-0 +37321-4 0 00004
2 22577 71.0378 114.2994 0116090 185.1746 249.0949 14.43895534 03
| Epoch (UTC): | 10 April 2026 01:54:19 |
| Eccentricity: | 0.0116090 |
| inclination: | 71.0378° |
| perigee height: | 663 km |
| apogee height: | 828 km |
| right ascension of ascending node: | 114.2994° |
| argument of perigee: | 185.1746° |
| revolutions per day: | 14.43895534 |
| mean anomaly at epoch: | 249.0949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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