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 67017U 26145.35625307 +.00000000 +00000-0 +24739-3 0 00001
2 67017 70.0007 261.0719 0003242 271.0166 89.0622 14.98335392 01
| Epoch (UTC): | 25 May 2026 08:33:00 |
| Eccentricity: | 0.0003242 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 261.0719° |
| argument of perigee: | 271.0166° |
| revolutions per day: | 14.98335392 |
| mean anomaly at epoch: | 89.0622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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