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 51846U 26144.96650676 +.00000000 +00000-0 +91057-3 0 00004
2 51846 97.3634 239.8544 0005166 216.8287 143.2630 15.86946634 06
| Epoch (UTC): | 24 May 2026 23:11:46 |
| Eccentricity: | 0.0005166 |
| inclination: | 97.3634° |
| perigee height: | 307 km |
| apogee height: | 314 km |
| right ascension of ascending node: | 239.8544° |
| argument of perigee: | 216.8287° |
| revolutions per day: | 15.86946634 |
| mean anomaly at epoch: | 143.2630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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