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 45759U 26145.49158122 +.00000000 +00000-0 +74831-3 0 00009
2 45759 53.0465 192.2314 0007290 344.9671 15.1125 15.62788968 04
| Epoch (UTC): | 25 May 2026 11:47:52 |
| Eccentricity: | 0.0007290 |
| inclination: | 53.0465° |
| perigee height: | 375 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 192.2314° |
| argument of perigee: | 344.9671° |
| revolutions per day: | 15.62788968 |
| mean anomaly at epoch: | 15.1125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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