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 67036U 26145.47880369 +.00000000 +00000-0 +77367-3 0 00001
2 67036 42.9993 324.3648 0000458 271.4099 88.6700 15.27591337 01
| Epoch (UTC): | 25 May 2026 11:29:28 |
| Eccentricity: | 0.0000458 |
| inclination: | 42.9993° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 324.3648° |
| argument of perigee: | 271.4099° |
| revolutions per day: | 15.27591337 |
| mean anomaly at epoch: | 88.6700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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