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 67041U 26145.48651502 +.00000000 +00000-0 +33262-3 0 00009
2 67041 42.9972 324.4252 0000526 285.2419 74.8374 15.27606711 08
| Epoch (UTC): | 25 May 2026 11:40:34 |
| Eccentricity: | 0.0000526 |
| inclination: | 42.9972° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 324.4252° |
| argument of perigee: | 285.2419° |
| revolutions per day: | 15.27606711 |
| mean anomaly at epoch: | 74.8374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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