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 60925U 26144.67165927 +.00000000 +00000-0 +12789-4 0 00006
2 60925 53.1580 326.8777 0000687 91.1628 268.9468 15.69708928 02
| Epoch (UTC): | 24 May 2026 16:07:11 |
| Eccentricity: | 0.0000687 |
| inclination: | 53.1580° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 326.8777° |
| argument of perigee: | 91.1628° |
| revolutions per day: | 15.69708928 |
| mean anomaly at epoch: | 268.9468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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