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 67472U 26145.41310392 +.00000000 +00000-0 +43488-3 0 00000
2 67472 43.0019 132.1317 0001358 267.2166 92.8530 15.27607904 08
| Epoch (UTC): | 25 May 2026 09:54:52 |
| Eccentricity: | 0.0001358 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.1317° |
| argument of perigee: | 267.2166° |
| revolutions per day: | 15.27607904 |
| mean anomaly at epoch: | 92.8530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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