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 67118U 26145.55091841 +.00000000 +00000-0 +56883-3 0 00000
2 67118 42.9934 94.6987 0002440 278.3372 81.7203 15.27601423 03
| Epoch (UTC): | 25 May 2026 13:13:19 |
| Eccentricity: | 0.0002440 |
| inclination: | 42.9934° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 94.6987° |
| argument of perigee: | 278.3372° |
| revolutions per day: | 15.27601423 |
| mean anomaly at epoch: | 81.7203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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