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 62067U 26145.12471405 +.00000000 +00000-0 +18668-2 0 00007
2 62067 53.1567 54.8151 0000892 85.8299 274.2821 15.69778605 04
| Epoch (UTC): | 25 May 2026 02:59:35 |
| Eccentricity: | 0.0000892 |
| inclination: | 53.1567° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 54.8151° |
| argument of perigee: | 85.8299° |
| revolutions per day: | 15.69778605 |
| mean anomaly at epoch: | 274.2821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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