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 67518U 26145.57379373 +.00000000 +00000-0 +53190-3 0 00003
2 67518 43.0037 239.9020 0001015 276.8842 83.1894 15.27587138 05
| Epoch (UTC): | 25 May 2026 13:46:15 |
| Eccentricity: | 0.0001015 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 239.9020° |
| argument of perigee: | 276.8842° |
| revolutions per day: | 15.27587138 |
| mean anomaly at epoch: | 83.1894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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