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 67509U 26145.62262542 +.00000000 +00000-0 +53403-3 0 00005
2 67509 42.9999 240.3006 0001464 269.6126 90.4558 15.27586033 04
| Epoch (UTC): | 25 May 2026 14:56:34 |
| Eccentricity: | 0.0001464 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.3006° |
| argument of perigee: | 269.6126° |
| revolutions per day: | 15.27586033 |
| mean anomaly at epoch: | 90.4558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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