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 60753U 26088.01683025 +.00000000 +00000-0 +93531-3 0 00007
2 60753 89.0602 289.4602 0111838 99.1456 262.2401 14.09239323 08
| Epoch (UTC): | 29 March 2026 00:24:14 |
| Eccentricity: | 0.0111838 |
| inclination: | 89.0602° |
| perigee height: | 781 km |
| apogee height: | 943 km |
| right ascension of ascending node: | 289.4602° |
| argument of perigee: | 99.1456° |
| revolutions per day: | 14.09239323 |
| mean anomaly at epoch: | 262.2401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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