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 62754U 26145.52962367 +.00000000 +00000-0 +67685-3 0 00000
2 62754 43.0003 80.0454 0000683 55.1108 304.9808 15.27582200 08
| Epoch (UTC): | 25 May 2026 12:42:39 |
| Eccentricity: | 0.0000683 |
| inclination: | 43.0003° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.0454° |
| argument of perigee: | 55.1108° |
| revolutions per day: | 15.27582200 |
| mean anomaly at epoch: | 304.9808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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