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 25544U 26064.77024645 +.00000000 +00000-0 +15013-3 0 00009
2 25544 51.6317 91.7338 0008144 160.7168 199.4130 15.48462755 06
| Epoch (UTC): | 05 March 2026 18:29:09 |
| Eccentricity: | 0.0008144 |
| inclination: | 51.6317° |
| perigee height: | 416 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 91.7338° |
| argument of perigee: | 160.7168° |
| revolutions per day: | 15.48462755 |
| mean anomaly at epoch: | 199.4130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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