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 67513U 26145.53796905 +.00000000 +00000-0 +79355-3 0 00009
2 67513 43.0001 240.5022 0000780 277.1186 82.9577 15.27614757 07
| Epoch (UTC): | 25 May 2026 12:54:40 |
| Eccentricity: | 0.0000780 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 240.5022° |
| argument of perigee: | 277.1186° |
| revolutions per day: | 15.27614757 |
| mean anomaly at epoch: | 82.9577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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