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 26066.51273615 +.00000000 +00000-0 +27602-3 0 00003
2 25544 51.6318 83.1189 0008132 167.0679 193.0520 15.48507964 05
| Epoch (UTC): | 07 March 2026 12:18:20 |
| Eccentricity: | 0.0008132 |
| inclination: | 51.6318° |
| perigee height: | 416 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 83.1189° |
| argument of perigee: | 167.0679° |
| revolutions per day: | 15.48507964 |
| mean anomaly at epoch: | 193.0520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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