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 45442U 26145.61116209 +.00000000 +00000-0 -15453-2 0 00007
2 45442 87.8913 25.5591 0001715 80.7339 279.3982 13.11414521 01
| Epoch (UTC): | 25 May 2026 14:40:04 |
| Eccentricity: | 0.0001715 |
| inclination: | 87.8913° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5591° |
| argument of perigee: | 80.7339° |
| revolutions per day: | 13.11414521 |
| mean anomaly at epoch: | 279.3982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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