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 67035U 26145.50836054 +.00000000 +00000-0 +59028-3 0 00000
2 67035 43.0012 324.5880 0001528 266.5341 93.5336 15.27589883 01
| Epoch (UTC): | 25 May 2026 12:12:02 |
| Eccentricity: | 0.0001528 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.5880° |
| argument of perigee: | 266.5341° |
| revolutions per day: | 15.27589883 |
| mean anomaly at epoch: | 93.5336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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