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 21775U 26140.29348774 +.00000000 +00000-0 +00000-0 0 00002
2 21775 63.3476 221.7564 3340816 273.0927 49.9774 5.53396299 06
| Epoch (UTC): | 20 May 2026 07:02:37 |
| Eccentricity: | 0.3340816 |
| inclination: | 63.3476° |
| perigee height: | 2613 km |
| apogee height: | 11634 km |
| right ascension of ascending node: | 221.7564° |
| argument of perigee: | 273.0927° |
| revolutions per day: | 5.53396299 |
| mean anomaly at epoch: | 49.9774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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