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 60119U 26145.41118071 +.00000000 +00000-0 +30742-5 0 00002
2 60119 53.1593 203.0255 0001182 72.3398 287.7749 15.69703278 08
| Epoch (UTC): | 25 May 2026 09:52:06 |
| Eccentricity: | 0.0001182 |
| inclination: | 53.1593° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 203.0255° |
| argument of perigee: | 72.3398° |
| revolutions per day: | 15.69703278 |
| mean anomaly at epoch: | 287.7749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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