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 60553U 26145.17060941 +.00000000 +00000-0 +83838-4 0 00002
2 60553 97.6809 220.9852 0008689 154.1509 206.0148 14.96085346 01
| Epoch (UTC): | 25 May 2026 04:05:40 |
| Eccentricity: | 0.0008689 |
| inclination: | 97.6809° |
| perigee height: | 573 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 220.9852° |
| argument of perigee: | 154.1509° |
| revolutions per day: | 14.96085346 |
| mean anomaly at epoch: | 206.0148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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