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 67026U 26145.33972008 +.00000000 +00000-0 +33749-3 0 00003
2 67026 70.0007 261.0120 0003327 270.1169 89.9609 14.98339206 06
| Epoch (UTC): | 25 May 2026 08:09:11 |
| Eccentricity: | 0.0003327 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 261.0120° |
| argument of perigee: | 270.1169° |
| revolutions per day: | 14.98339206 |
| mean anomaly at epoch: | 89.9609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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