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 63652U 26145.41744749 +.00000000 +00000-0 +71861-3 0 00009
2 63652 42.9992 291.6898 0001741 289.2245 70.8418 15.27593450 06
| Epoch (UTC): | 25 May 2026 10:01:07 |
| Eccentricity: | 0.0001741 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.6898° |
| argument of perigee: | 289.2245° |
| revolutions per day: | 15.27593450 |
| mean anomaly at epoch: | 70.8418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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