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 60722U 26145.16509808 +.00000000 +00000-0 +56957-5 0 00002
2 60722 53.1584 99.4633 0000948 65.5836 294.5281 15.69707801 08
| Epoch (UTC): | 25 May 2026 03:57:44 |
| Eccentricity: | 0.0000948 |
| inclination: | 53.1584° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 99.4633° |
| argument of perigee: | 65.5836° |
| revolutions per day: | 15.69707801 |
| mean anomaly at epoch: | 294.5281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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