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 45668U 26145.09655855 +.00000000 +00000-0 +11605-2 0 00008
2 45668 53.0519 80.0957 0002966 71.5120 288.6194 15.13469794 09
| Epoch (UTC): | 25 May 2026 02:19:02 |
| Eccentricity: | 0.0002966 |
| inclination: | 53.0519° |
| perigee height: | 524 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 80.0957° |
| argument of perigee: | 71.5120° |
| revolutions per day: | 15.13469794 |
| mean anomaly at epoch: | 288.6194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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