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 21574U 26153.63771116 +.00000000 +00000-0 +12191-3 0 00008
2 21574 98.7801 173.9799 0030965 311.7626 48.0915 14.39508009 04
| Epoch (UTC): | 02 June 2026 15:18:18 |
| Eccentricity: | 0.0030965 |
| inclination: | 98.7801° |
| perigee height: | 738 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 173.9799° |
| argument of perigee: | 311.7626° |
| revolutions per day: | 14.39508009 |
| mean anomaly at epoch: | 48.0915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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