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 21575U 26053.71340435 +.00000000 +00000-0 +74651-4 0 00003
2 21575 98.3630 124.5325 0007779 152.2378 207.9228 14.42316094 05
| Epoch (UTC): | 22 February 2026 17:07:18 |
| Eccentricity: | 0.0007779 |
| inclination: | 98.3630° |
| perigee height: | 745 km |
| apogee height: | 756 km |
| right ascension of ascending node: | 124.5325° |
| argument of perigee: | 152.2378° |
| revolutions per day: | 14.42316094 |
| mean anomaly at epoch: | 207.9228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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