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 60333U 26145.51570801 +.00000000 +00000-0 -58406-4 0 00001
2 60333 53.1604 79.0541 0001031 79.6792 280.4325 15.30175788 06
| Epoch (UTC): | 25 May 2026 12:22:37 |
| Eccentricity: | 0.0001031 |
| inclination: | 53.1604° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 79.0541° |
| argument of perigee: | 79.6792° |
| revolutions per day: | 15.30175788 |
| mean anomaly at epoch: | 280.4325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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