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 26088.23139301 +.00000000 +00000-0 +60243-4 0 00001
2 22577 71.0392 140.3373 0116868 204.0348 223.1325 14.43890667 05
| Epoch (UTC): | 29 March 2026 05:33:12 |
| Eccentricity: | 0.0116868 |
| inclination: | 71.0392° |
| perigee height: | 662 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 140.3373° |
| argument of perigee: | 204.0348° |
| revolutions per day: | 14.43890667 |
| mean anomaly at epoch: | 223.1325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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