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 56170U 26088.15831197 +.00000000 +00000-0 +51931-4 0 00004
2 56170 81.0037 157.2296 0011034 150.5051 209.6730 13.86152254 02
| Epoch (UTC): | 29 March 2026 03:47:58 |
| Eccentricity: | 0.0011034 |
| inclination: | 81.0037° |
| perigee height: | 934 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 157.2296° |
| argument of perigee: | 150.5051° |
| revolutions per day: | 13.86152254 |
| mean anomaly at epoch: | 209.6730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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