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 60554U 26145.13988649 +.00000000 +00000-0 +20579-3 0 00005
2 60554 97.6649 223.2513 0003801 98.5055 261.6600 15.00920395 00
| Epoch (UTC): | 25 May 2026 03:21:26 |
| Eccentricity: | 0.0003801 |
| inclination: | 97.6649° |
| perigee height: | 561 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 223.2513° |
| argument of perigee: | 98.5055° |
| revolutions per day: | 15.00920395 |
| mean anomaly at epoch: | 261.6600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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