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 51860U 26145.10328906 +.00000000 +00000-0 +67685-4 0 00006
2 51860 53.2129 26.0836 0001244 80.5508 279.5624 15.08827669 03
| Epoch (UTC): | 25 May 2026 02:28:44 |
| Eccentricity: | 0.0001244 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 26.0836° |
| argument of perigee: | 80.5508° |
| revolutions per day: | 15.08827669 |
| mean anomaly at epoch: | 279.5624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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