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 62524U 26145.47277804 +.00000000 +00000-0 +56498-3 0 00004
2 62524 43.0011 146.0634 0001825 262.7557 97.3087 15.27596482 07
| Epoch (UTC): | 25 May 2026 11:20:48 |
| Eccentricity: | 0.0001825 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.0634° |
| argument of perigee: | 262.7557° |
| revolutions per day: | 15.27596482 |
| mean anomaly at epoch: | 97.3087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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