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 26144.44963014 +.00000000 +00000-0 +00000-0 0 00003
2 21775 63.3476 220.0503 3340026 273.0939 49.9788 5.53396536 06
| Epoch (UTC): | 24 May 2026 10:47:28 |
| Eccentricity: | 0.3340026 |
| inclination: | 63.3476° |
| perigee height: | 2614 km |
| apogee height: | 11633 km |
| right ascension of ascending node: | 220.0503° |
| argument of perigee: | 273.0939° |
| revolutions per day: | 5.53396536 |
| mean anomaly at epoch: | 49.9788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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